PORFLOW - a model for fluid flow, heat and mass transport in multifluid, ======= multiphase, fractured or porous media Analytic & Computational Reasearch Inc. 3106 Inglewood Boulevard West Los Angeles CA 90066 (213) 398-0956 European distributor: ACRI ( http://www.acri.fr/) Mecanique Appliquee et Sciences de l'environnement 260, route du Pin Montard - B.P. 234 06904 Sophia Antipolis Cedex FRANCE Tel : +33 (0)4 92 96 75 00 Fax : +33 (0)4 93 95 80 98
The Science and Technical Software Company
Electronic Publishers and Distributors
8201 Corporate Drive, Suite 1110
Landover, Maryland 20785
FAX (301) 459-3776
What is TEP?
Note: COSMIC/NASA is no more: they closed the summer of 1998.
of commercial software.
Fluent Inc. /
Centerra Resource Park
10 Cavendish Court
Lebanon, NH 03766-1442
tel: 603.643.2600, 800.445.4454
Fluent Inc. distributors around the world and CFD software packages. For more information contact info@Fluent.COM.
From Leif Broberg /
Flowtech International AB
Date: Fri, 24 Jan 1997 10:01:13 +0100 (MET)
S-400 22 Gothenburg
Flowtech International AB
SHIPFLOW. As the name suggests, this code is good for design/analysis of flow around ships. It uses a non-linear free surface panel method, a boundary layer method and a Reynolds averaged Navier-Stokes method to calculate wave-making resistance, skin friction resistance, sinkage etc for the modern Naval Architect. FLOWTECH International AB now can be contacted directly by e-mail and www. E-mail: firstname.lastname@example.org WWW: www.flowtech.se Phone: int.+46 31 41 05 06 Fax: int.+46 31 41 50 60
Fluid Dynamics International, Inc.
500 Davis Street, Suite 600
Evanston, IL 60201 USA
phone (708) 491-0200
fax (708) 869-6495
AEA Technology is one of the world's leading innovation businesses, turning science and engineering into profit for the benefit of its customers and investors. We have years of experience in understanding complex industrial processes and managing the way in which they interact with each other and their environment. It is the innovative delivery of our knowledge and skills that differentiates AEA Technology from its competitors.
The Engineering Software business of AEA Technology develops and markets the CFX family of software and services. CFX is a suite of powerful fluid engineering software tool that can be used to simulate many types of industrial flow and heat transfer processes. Continuous development ensures CFX's continued position at the forefront of CFD technology. From the outset it has been designed to be easy to use, robust, accurate and fast, providing new insights and better understanding of the most complex fluid flow processes. The CFX group also provides computational fluid engineering expertise in the form of consulting services for CFD design, development and analysis.
Code name: CFX UK Address Company: AEA Technology Engineering Software AEA Technology plc Address: 2927 West Liberty Avenue #183 8.19 Harwell, Didcot Pittsburgh, PA 15216 Oxfordshire OX11 0RA Telephone: (888) 827-2356 (44 1235) 433813 Fax: (519) 886-7580 (44 1235) 432989 E-Mail email@example.com Web Site http://www.aeat.com/cfx
From Wayne A. Christopher /
ICEM Technologies, GmbH and
ICEM CFD Engineering of Berkeley, CA
For more information contact firstname.lastname@example.org
ICEM Technologies, GmbH and
ICEM CFD can generate high-quality computational grids for CFD and other applications, based on either NURBS surfaces from CAD systems or existing surface meshes. It includes modules for generating:
Icepak includes an object-based modeling system, which allows users to rapidly create complex models with pre-defined component types, a fully automatic hexahedral grid generator that creates body-fitted high-quality grids, the Fidap flow solver, and extensive post-processing capabilities.
For more information, please take a look at our WWW page, or contact Mary Jo Hamilton (email@example.com, (508) 497-2341).
From R. Sukumar /
CFD Research Corporation
Date: Fri, 15 Dec 1995 14:01:56 -0800 (PST)
3325 Triana Blvd.
Huntsville, AL 35805
CFD Research Corporation
CFD-ACE Advanced General Purpose CFD Code CFD-FASTRAN High Accuracy Compressible Flow Solver on Unstructured, Structured, Hybrid Grids CFD-TWOPHASE Advanced multi-phase CFD solver CFD-GEOM Interactive 3D Geometry/Grid Generation Software CFD-VIEW Interactive 3D Graphics, Animation and Flow Visualization Software. For more information see www.cfdrc.com.
Article: 656 of sci.physics.computational.fluid-dynamics
From H.W. Krus / hwkrus@inter.NL.net
Subject: Re: Need addresses of Fidap/Fluent and others
Date: Tue, 26 Jul 1994 06:37:36 GMT
STAR-CD by Computational Dynamics, Limited. Homepage is www.cd.co.uk.
AMI has a web page at http://www.am-inc.com AMI was incorporated in 1971 to conduct research and development in aerodynamics and hydrodynamics for government and industry. Since then AMI has developed a series of robust CFD codes that can be applied to a wide range of practical problems. AMI also markets and provides technical support for some CFD codes written by others under cooperative agreements with the original authors. AMI headquarters is located in Redmond, WA. The Arlington, VA office specializes in hydrodynamic applications of CFD technology. AMI has marketing and support agreements with companies in Europe, Asia, and Australia. Some of the codes available from AMI include: -VSAERO: A full configuration, subsonic aeroynamics analysis method that solves the linearized potential flow equations. VSAERO uses piecewise constant singularity strengths on surface panels to represent arbitrary three-dimensional configurations. Boundary layer calculations can be performed along on-body streamlines and the resulting boundary layer thicknesses can be used to iteratively correct the inviscid flowfield (using surface transpiration). Compressibility corrections are available within the program for higher subsonic Mach number cases. Wake geometry is determined by an iterative wake shape calculation procedure. Special purpose modules such as; FSWAVE, ROTOR and PROPFAN expand VSAERO's capabilities. These modules calculate the nonlinear hydodynamic wave effects on surface piercing vessels, helicopter rotor/fuselage interactions and propeller/fan performance, respectively. -FSWAVE: A free-surface module developed for VSAERO which uses desingularized source panels raised above the free water surface combined with normal VSAERO (source and dipole) panels on the ship hull surface to predict the steady flow past submerged or floating vehicles. Provisions are made for predicting the change in the draft and trim of a ship resulting from its forward speed, to model the flow past a transom stern, to model the flow past a ship traveling in shallow water, and to model the flow past lifting surfaces near a free surface. The program satisfies the nonlinear boundary condition on the free water surface. This is done in an iterative manner, where during each iteration the linearized solution about the flow resulting from the previous iteration is computed using an approach similar to that originally developed by Dawson. The first iteration solves for the flow linearized about the free stream flow. -USAERO: This program calculates the transient aerodynamic characteristics of complex configurations in arbitrary motion. It is based on a time-stepping procedure which allows relative motions of configuration components. USAERO simulations include manuevering aircraft, gust response, rotor/body interactions and stores separation from aircraft. Special application modules FPI and FSP couple with USAERO to provide flight-path integration calculations with six degrees of freedom and ship motion calculations with nonlinear free-surface simulation. -MGAERO: A 3-D Euler method for computing flow about arbitrary configurations in the subsonic through supersonic flight regimes. It uses a multigrid approach with an equally-spaced Cartesian mesh structure including local refinement. Swept, unswept and rotated grids may be used to develop local computational domains which may be overlapped with either the surface or other multigrid levels. The ease of geometry and grid input allows for rapid turnaround of results for complete aircraft, including nacelles. -OMNI3D: A color graphics visualization program which displays simulation results in 3-D and arbitrary 2-D slices. It shows surface pressure, velocity and Mach number contours on the body and in the flow field, streamline and boundary-layer parameters along on- and off-body streamline trajectories and wake geometry data. Time steps and iterations may be animated or stepped through. OMNI3D's mouse-driven interface and fast graphics permit rapid assessment of results on complex configurations. -ICE: This code calculates particle trajectories in the vicinity of an arbitrary aircraft for use in icing and sand-ingestion analyses. The efficient trajectory calculation and prescribed velocity field result in a very fast calculation. ICE reads the aircraft geometry and flowfield velocity from an OMNI3D graphics file. -XFOIL: An interactive program for the design and analysis of subsonic airfoils. It consists of a collection of menu-driven routines which perform functions such as; viscous (or inviscid) analysis of an existing airfoil, airfoil design and redesign by interactive specification of a surface speed distribution, airfoil redesign by interactive specification of new geometric parameters. XFOIL is based upon a linear-vorticity stream function panel method, coupled to a two-equation, lagged dissapation integral boundary layer formulation. -MSES: A coupled viscous/inviscid Euler method for the analysis and design of multi-element (and single-element) airfoils. A streamline-based Euler discretization and a two-equation integral boundary layer formulation are coupled through the displacement thickness and solved simultaneously by a full Newton method. MSES is capable of multi-point optimization of single- and multi-element airfoils. The full Newton solution method of the solver permits effectively "free" calculation of the flowfield sensitivities to predefined element shape deformation modes and element translation and rotation modes. -MISES: A coupled viscous/inviscid Euler method for the analysis an design of cascades. The internal formulation of this code is much like that of MSES's. -CAMRAD II: An aeromechanical analysis of helicopters and rotorcraft that incorporates a combination of advanced technology, including multibody dynamics, nonlinear finite elements, structural dynamics and rotorcraft aerodynamics. For the design, testing and evaluation of rotors and rotorcraft, CAMRAD II calculates performance, loads, vibration, response and stability. -INCA: A compressible Navier-Stokes flow solver with turbulence and chemistry modelling options. An advanced solution procedure is used to solve the equations on multi-block, body-fitted, finite-volume computational grids. Subsonic, transonic, supersonic, and hypersonic viscous flows can be calculated for complex geometries. For pricing inquiries, contact Frank Dvorak, email firstname.lastname@example.org For technical questions concerning aerodynamic applications, contact David Lednicer, email email@example.com For technical questions concerning hydrodynamic applications, contact Burke Murray, email firstname.lastname@example.org For technical questions about FSWAVE, contact Mike Hughes, email email@example.com Seattle office: Analytical Methods, Inc. 2133 152nd Ave NE Redmond, WA 98052 USA (425) 643-9090 Virginia Office: Analytical Methods, Inc. 1110 N. Glebe Rd., Suite 1050 Arlington, VA 22207 USA (703) 522-5728
From Eric J. Fuller /
Date: Wed, 5 Nov 1997
AeroSoft currently markets and supports the state-of-the-art, computational fluid dynamics code, General Aerodynamic Simulation Program (GASP). GASP is well suited for a wide range of fluid dynamics applications, and in particular for military applications due to its extensive thermo-chemical library. GASP's thermo-chemical library allows users to model complex fluid dynamic phenomena including frozen, equilibrium, and finite-rate chemistry as well as non-equilibrium thermodynamics. The extensive variety of physical models incorporated into GASP provides a complete tool for modeling complex three-dimensional steady or time-dependent flows throughout the performance envelope. Because of the broad flexibility inherent in this software, and its wide acceptance and use by the defense industry, GASP is an ideal target for the scalable parallel computing environment.
AeroSoft's next generation of simulation tools is based on an unstructured finite-volume formulation. In the General Unstructured Software Toolkit (GUST) the majority of physical modeling capabilities currently distributed with GASP are also supported. Both the structured and unstructured packages share a common library of routines used to calculate such quantities as thermodynamic and transport properties, inviscid fluxes, and source terms for the finite-rate chemical reactions. GUST is capable of accurately simulating time-dependent problems whose domain can be described with a single grid and single connectivity array. The unstructured code is highly optimized for vectorization on Cray supercomputers and parallelization via decomposition on distributed memory multiprocessor architectures.
1872 Pratt Drive, Suite 1275
Blacksburg, VA 24060-6363
From Andrew Norris /
Date: Wed, 7 Sep 1994 10:03:59 -0400
Product: FLOW-3D v7.1
Author/Company: Flow Science, Inc.
Location: Los Alamos, NM
Methodology: Finite Difference, VOF, FAVOR
Special Features: Free Surfaces, Saturated/Unsaturated Porous Media,
Chemistry, Solidification, Cavitation, Moving Obstacles, Bubbles.
Availability: PC (DOS, Windows 95, Windows NT, UNIX, Mainfraimes)
From James D. Freels /
Date: Tue, 27 Sep 94 10:48 EDT
Reaction Engineering International
77 West 200 South
Salt Lake City, UT 84101
Voice: (801) 364-6925
FAX: (801) 364-6977
BANFF/GLACIER - specialize in simulating three dimensional combustion applications - marketed through REI based in SLC, UTAH. GLACIER is an extension of BANFF that includes turbulent particle dispersion and reaction. the cfd is done using a finite-volume approach and particles are coupled using a Lagrangian cloud formulation. -it can handle complex three-dimensional geometries -full coupling between turbulent fluid and particle mechanics , radiative and convective heat transfer and chemical reactions in multiple phases. - typical applications are burner and furnace design, utility boilers, waste incineration, pulverized coal combustion, other cfd applcations including those involving turbulent particle transport. We now have a page that describes the codes marketed by REI - the page is located at http://www.reaction-eng.com.
Article: 956 of sci.physics.computational.fluid-dynamics
From Albert Sulmistras / firstname.lastname@example.org
In article <email@example.com>, firstname.lastname@example.org (Mr.Door) writes: > Greetings, > Part of my PhD work involves the use of two-dimensional FCT codes to > simulate detonation phenomena. This work is now moving towards the > simulation of shocks/detonations passing over irregular obstacles > (say, shocks against wedges) which is something that my existing code > isn't too good at. SNIP... > o Are there any other schemes around which allow relatively > painless simulation of shocks over irregular obstacles - speed > isn't that much of an object, but accuracy is. Eulerian > schemes are preferred, since that's what I'm used to. If the objective is to model shocks and detonations in complex 2-D and 3-D geometries, the FE approach is NOT the only way to go. We (Combustion Dynamics) developed an Euler code using FCT 6th order in a rectilinear grid. Complex solid shapes can be defined in the calculation domain. We then detect all solid surfaces and use Reimann solvers across the boundary and impose free-slip conditions at the surface. The benefit being that the whole problem setup only requires several minutes... really :^) and you do not need complex grid generators. For a detonation model, we currently have one-step and two-step combustion models. For equilibrium or chemical kinetic modelling of shocks and detonations (i.e. ZND profile, CJ parameters, reflected shocks, etc.) you can let your big cheese (Geraint) know that a beta version of "SuperSTATE" will be heading his way shortly (depending on your definition of short :^) ). Regards, Albert
Tel.: +43 316 987-441
FAX : +43 316 987-777
FIRE is an in house development of AVL List Gmbh. FIRE is based on a finite volume differencing scheme using a modified variant of the SIMPLE algorithm for the solution of
Our FIRE Web Server has an extensive collection of information regarding FIRE. You are welcome to surf through our cyber space.
Mechanical Design and Analysis: Fluids, CFD, Flow Analysis
From Joy Crisp /
Date: Wed, 12 Oct 94 18:36:03 PDT
Computational Fluid Dynamics
From John R. Chawner /
Date: Wed, 2 Aug 1995 22:06:20 -0500
Gridgen is a software system for the generation of structured grids for use in the computational sciences. The grids generated by Gridgen consist of body-conforming, quadrilateral and hexahedral cells. Gridgen is capable of building multi- or single-block grids, abutting or overlapping blocks, surface or volume grids, and 2D or 3D grids. Gridgen consists of two codes, Gridgen (interactive) and Gridgen3D (batch). Gridgen is a visually oriented and interactive code in which user control is maintained through menu button selection, mouse point-and-click, and occasional text input. On-line help may be accessed anywhere within the code, providing both specific and general information to facilitate code usage. A User's Manual is also available with sections covering the theory, how-to, and a tutorial. The Gridgen process begins with import of the geometry model about which the grid is to be generated. The geometry model may be imported in a variety of formats including IGES. Imported geometry may be supplemented by geometry created in Gridgen. Next, the user interactively creates the curve, surface, and volume grid components. Curves are constructed first as free space or model-constrained curves of various mathematical forms. Grid points are distributed along the curves using any of several clustering functions that allow for clustering anywhere along the curve's length. Surface grids are then initialized automatically after the user selects the curves that define the surface's perimeter. Surface grid point refinement may be achieved by applying a suite of techniques from Gridgen's broad algebraic and elliptic partial differential equation functionality. Volume grids are constructed in a similar manner, by interactively selecting the surface grids that comprise the block boundary. Volume grid points are initialized automatically and may be refined by accessing Gridgen3D, a 3D partial differential equation code run in batch mode. Interfaces to the TEAM, NPARC, OVERFLOW, CNSFV, DTNS, FANS, VSAERO, and INCA analysis codes are included in Gridgen. These interfaces allow users to set solver-specific boundary conditions on the surfaces of the blocks in the system. The final products of Gridgen, the grid and connection/boundary condition input decks, can then be exported in the exact form required by the flow solvers. Gridgen runs on all Silicon Graphics workstations including those with 8-bit graphics. Now 11 years old and 300+ users strong, Gridgen development and support today is maintained by its two original authors, John Steinbrenner and John Chawner, of Pointwise, Inc., Bedford, Texas. For licensing information please contact John Chawner at (817) 354-1004, email@example.com, or http://www.pointwise.com.
From Jean-Philippe Moins /
Date: Tue Feb 20 13:44:18 MET 1996
1, rue James Joule
Simulog offers a complete CFD software solution including Simail, structured/unstructured mesh generator, N3S (finite element) and ESTET-ASTRID (finite volume, two-phase flows) CFD solvers and EnSight, an advanced post-processor by Computational Engineering, Inc. Click for product information in French or in English. For more information, please contact firstname.lastname@example.org.
From Murali /
Date: Tue, 22 Nov 1994 10:22:08 +0700 (SST)
From Juliusz Kirejczyk /
Date: Sat, 17 Dec 1994 20:33:04 -0800
FLOTRAN, ANSYS, Inc. finite element method, integrated with ANSYS pre/postprocessor
From Brian Pospichal /
Date: Thu, 16 Feb 1995 10:52:42 -0600
FLOTHERM FLOTHERM is designed to provide an analysis tool for all aspects of thermal problems arising in electronic equipment. It is particularly powerful in cases where convective cooling is domonant or critical. It provides complete analysis of the flow of cooling fluid (usually air) simultaneously with thermal analysis. FLOTHERM handles thermal and fluid dynamic behavior for: * 2D and 3D * steady and transient * laminar and turbulent * forced and natural convection * convection,conduction and (to an extent) radiation. * conjugate heat transfer FLOTHERM is based on techniques of CFD, specifically the Finite Control Volume approach. * It operates in cartesian coordinates * Calculation is performed in a rectangular cuboid solution domain * Solution requires calculation throughout the domain of the variables: - fluid (air) velocities in the x, y and z directions (u,v and w) - fluid static pressure (p) - temperature of fluid and, if required, in solid regions (T) The variables are in general functions of x,y and z, and time t. FLOTHERM is available, commercially, from: Corporate Headquarters- Flomerics Limited 81 Bridge Road Hampton Court Surrey KT8 9HH England North American Office- Gerard J. Kates Flomerics, Inc. Sales Manager, Eastern Region 2 Mount Royal Avenue Marlboro, MA 01752 Tel# 508-460-0112 Fax# 508-624-0559 E-mail: email@example.com Web Page: www.flomerics.com
From James D. Freels /
Date: Tue, 27 Sep 94 10:48 EDT
Any one who is interested in computational mechanics and do not like to write lengthy codes to get a solution should try the new AKCESS.* platform. For a brief overview look into the WWW mosaic page at http://cmc2.akcess.com/.
Computational Mechanics Company,Inc. (COMCO).
Storesim/Tetmesh a Multi-Body CFD Grid Generation and Flow Solution Software
Unisim a Two-Phase Reservoir Simulator built using PHLEX, a multipurpose hp-adaptive, vector/parallel finite element kernel.
KASIMIR: The program is commercially available from the Shock Wave Laboratory. If you need more information, please contact Michael Lenartz, e-mail address: firstname.lastname@example.org.
Date: Tue, 28 Mar 95 14:14:21 +0900
From Stephen Kramer /
Date: Mon, 27 Mar 1995 13:27:58 -0700
NUMECA develops and markets a new generation of software products for fast, accurate and cost-effective Computational Fluid Dynamics. NUMECA's software products include :
NUMECA also markets FINE/Design for the rapid design and optimization of blades and channels including Blade-to-blade, Throughflow and inverse CFD methods.
NUMECA's website (http://www.numeca.com) gives more detailed information about the company and its software products.
Our address is :
Numeca International s.a.
5, Av. Franklin Roosevelt
TEL: +32 2 647 83 11
FAX : +32 2 647 93 98
The contact person is :
CEI Inc. /
PO Box 14306
Research Triangle Park, NC 27709 USA
tel: (919) 481-4301
fax: (919) 481-4306
EnSight is an advanced CFD postprocessing package with a unique distibuted architecture. For more information, CEI, Inc. or email@example.com.
fax +46 46 136264
Dag Hammarskjolds vag 5C
S-224 64 LUND
fax +46 46 136264
We also have about 30 other PC-programs for building physics applications, such as heat transfer, moisture, air, energy balances, and ground heat storage. (Keywords: Building Physics, Building Technology, Civil Engineering, Mechanical Engineering, Physics, Energy, Heat transfer, Ground heat storage, Computer software.)
HEAT2is a user-friendly PC-program for two-dimensional transient and steady-state heat transfer. A wide range of heat transfer problems may be solved. The program handles the following internal modifications: heat sources and areas with a given temperature (constant in time or sinusoidal, step-wise constant, or step-wise linear); cavities with air (radiation and ventilation); cavities with a fluid of a single temperature; internal resistances. In the standard version 15625 (125*125) computational nodes may be used.
HEAT2solves the heat conduction equation by the method of explicit finite differences. Authors: Thomas Blomberg, Johan Claesson For more information, see our homepage http://www.blocon.se. Blocon Software Agency ---------------------
HEAT3is a PC-program for three-dimensional transient and steady-state heat transfer. A wide range of heat transfer problems may be solved.
HEAT3has optimized 32-bit protected mode code. This gives high calculation speed and allows for memory allocation for large three-dimensional problems. Up to one million computational nodes (1000000) may be used on a PC with 32 Mb RAM.
HEAT3solves the heat conduction equation by the method of explicit finite differences. Authors: Thomas Blomberg, Johan Claesson For more information, see our homepage http://www.blocon.se. Blocon Software Agency ---------------------
Our domain is http://www.blocon.se
Adaptive Research Division
Adaptive Research Corporation Adaptive Research offers an advanced computational fluid dynamics software system for UNIX workstations, supercomputers, and high-performance PCs. CFD2000 is a fully-integrated software system providing a common interface (based on a sophisticated 3D windowing scheme) to our automatic mesh generators, the powerful Storm flow solver, and advanced scientific visualization capability. Adaptive Research Division 4960 Corporate Drive, Suite 100-A 2900 28th St #300 Huntsville, AL 35805 Santa Monica, CA 90405 Phone: (205)-830-2620 Phone: (800)-326-5155 Fax: (205)-830-2628 Fax: (310)-314-2323 firstname.lastname@example.org http://www.adaptive-research.com
From Alan Hsing /
Unicom Technology Systems
2721 Bishop Street
Lawrence, KS 66046
We like to introduce VORSTAB-PC, an aerodynamic code based on quasi-vortex- lattice method and written in Fortran-77, compiled and optimised for 486 PCs. Very handy for applied aerodynamic calculations, flight dynamics studies or preliminary aero designs. Requires only 486 with 8mb ram/5mb hd space/DOS 5+. It deals with lifting surfaces such as wings, vertical tails, horizontal tails, leading-edge flaps, straks, ailerons, trailing-edge flaps, winglets, and fuselage, body of revolution, body with irregular cross-section shape and user definable wing cambers, twisting, tapered wings and airfoil thickness. It covers both subsonic and supersonic (compressible folw) flows, and includes asymmetrical forebody vortex separation, vortex breakdown effect and vortex wake effect, etc. It computes all the longitudinal characteristics & 9 lateral-directional stability parameters and pitch damping derivatives at pre- & post-stall conditions, also high angle-of-attack characteristics, both in- & out-ground effects, hinge moment, torsional moment & bending moment distributions on lifting surfaces. It provides interactive input preparation with built-in graphical viewing of geometries and computed results. Special educational and volume discount are avaialble. A 30-day fully functional demo disk (1.44M) is available for $5 shipping. There is also public domain version of VORSTAB-PC.
Incinerator Consultants Incorporated
11204 Longwood Grove Drive
Reston, Virginia 22094-1302 USA
Phone: 703/437-1790, FAX: 703/437-9048
ICI01, ICI02, ICI03, ICI04, ICI05, ICI06, ICI07 ABSTRACT: A series of heat balance programs for analysis of the design and operation of incineration systems. DESCRIPTIONS: These program packages includes generic programs in either Metric or American units, programs for rotary kiln incineration systems, fluid bed incinerators, and starvged-air process, commonly used for medical waste disposal. AUTHOR: These programs were developed by the consulting engineer Calvin R. Brunner, the author of ten texts on incineration and other waste disposal process, who is currently preparing his eleventh text titled MEDICAL WASTE DIPOSAL. REFERENCES: Programs are based on the techniques developed in Mr. Brunner's texts HANDBOOK OF INCINERATION SYSTEMS (McGraw Hill, 1991) and HAZARDOUS WASTE INCINERATION (McGraw Hill, 1993). AVAILABILITY: Commercial. Detailed program descriptions and costs are included on a DEMONSTRATION DISK. Contact INCINERATOR CONSULTANTS INCORPORATED to obtain a free DEMO DISK.
Concentration Heat & Momentum Ltd (CHAM)
40 High Street
Tel: + 44 (0) 181 947 7651
Fax: + 44 (0) 181 879 3497
CHAM, developers and worldwide distributors of PHOENICS CFD software. For an overview of CHAM's CFD software products go to: http://www.cham.co.uk or contact us via email at: email@example.com
From Alex Portalatin /
Date: Wed, 30 Aug 95 13:32:23 -0700
Date: Thu, 28 Sep 95 16:08:08 -0700
AVIA is a powerful 3-D Aero/Hydro interactive analysis & design system based on panel methods. Aplications range from 2-D profile analysis & generation to integrated 3-D body/wing/tail analysis.with boundary layer interaction. Also applicable to Sail design. For more information see http://www.gate.net/~avia/.
Phone: (510) 373-0628
XYZ Scientific Applications, Inc.
1324 Concannon Blvd.
Livermore, CA. 94550
FAX: (510) 373-6326
Phone: (510) 373-0628
TrueGrid is a commercial code designed to build large, complex fluid and structural meshes using hexahedron brick elements, quadralaterial shell elements, and beam elements. We support both linear and quadratic elements. The mesh is block structured and builds quality meshes is a short period of time. It is available on UNIX workstations and the PC.
Bruce Rosen, President
South Bay Simulations, Inc.
44 Sumpwams Avenue
Babylon, NY 11702 USA
Tel/Fax: (516) 587-3770
PHASES Engineering Solutions
Professor G. F. Naterer
Winnipeg, Manitoba, Canada
Professor G. F. Naterer
PHASES is a general purpose software package which numerically simulates fluid flow and heat - mass transfer processes in engineering applications. PHASES features include: (i) incompressible, two-phase and multiconstituent flow models, (ii) Windows95, Windows 3.1 and Windows NT compatibility, (iii) 32 bit compiler source code execution, (iv) realtime simulations, (v) powerful graphics libraries and data editors, (vi) finite element mesh generation with mouse-driven commands and (vii) several numerical analysis utilities. The numerical method employs finite volume - element models, implicit solutions, collocated variable storage and a simultaneous velocity - pressure coupling. The two-phase flow models incorporate a homogeneous, mixture formulation which includes species transport and elliptic grid transformations for volumetric shrinkage / expansion flows during solid - liquid phase transition. PHASES has special applications in materials processing industries. Additional industrial applications appear in fields such as aerodynamics, external flows, heat exchanger design, internal flows in pipes and ducts and heat transfer in buildings. Further information is available from Dr G. F. Naterer, Winnipeg, Manitoba, Canada, e-mail: firstname.lastname@example.org
Dave Taflin / email@example.com
phone: (206)827-3304 x210
phone: (206)827-3304 x210
Amtec Engineering, Inc., of Bellevue, WA, markets two CFD-related programs. INCA is a 3D multi-block structured-grid CFD solver for compressible ideal gas, with options for both non-equillibrium chemistry and incompressible flow. An implicit solver, it is ideally suited for high-speed, chemically reacting flow. It is available for Unix and DOS machines. Tecplot is an interactive data visualization program for structured and unstructured (finite-element type) data. Capabilities include wireframe, contour, vector, and streamline/ribbon plotting in 2D and 3D, 3D shaded plots, and data manipulation and animation. Version 7, due later this year, will be the first Windows/Motif version (Version 6 is DOS/Unix). Amtec's Web site is at http://www.amtec.com.
Article: 4633 of sci.physics.computational.fluid-dynamics
Engineering Sciences, Inc.
From Huan-Min Shang / shang@Hurricane.esi-al.com
Date: Fri, 24 May 1996 15:10:21 -0500
1900 Golf Road, Suite D, Huntsville, Alabama 35802
TEL: (205) 883-6233 / FAX: (205) 883-6267
Engineering Sciences, Inc.
We have a cfd code called UNIC that can run on PC, workstations, and supercomputers. If you are interested, you may visit our home page at http://www.esi-al.com.
Catalpa Research, Inc.
P. O. Box 3306, Champaign, IL 61826-3306
TEL: (217) 355-3365 / FAX: (217) 355-3365
TIGER CFD is designed specifically for turbomachinery CFD applications. Its customized grid generation package allows a user to obtain a high-quality grid within hours, instead of days or weeks.
For more information, please visit our site at http://www.catalpa.net
Alan M. Shih Email: Shih@Catalap.Net Staff Web : http://WWW.Catalpa.Net Catalpa Research, Inc. -- Hub of Turbomachinery CFD
Swansea NS codes
From Nick Lavery / N.P.Lavery@swansea.ac.uk
Date: Mon, 10 Jun 1996 17:49:22 +0100TURB are two FORTRAN codes (in 2-D and 3-D) which used k-l, k-epsilon and an ASM model of turbulence to solve the Reynolds Equations, coupled with a pseudo- transient time-stepping thermal equation solution. The solution uses the finite element method, and the codes are the result of over twenty years research by Professor Cedric Taylor at the Department of Civil Engineering here at Swansea. There is also an older code called LAM2D which solves the Navier-Stokes equations by the finite element method without any turbulence models. The sites at which they can be found are : http://www.swan.ac.uk/mecheng/staff/nlavery/code.html.
Engineering Systems International S.A.
From Pacific ESI / pesi@esi.COM.AU
Date: Sun, 16 Jun 1996 21:20:09 +1000
20 rue Saarinen
RUNGIS Cedex, 94588
FAX: 33-1-46-87-72-02 (fax)
Vince Chaillou - ESI / firstname.lastname@example.orgPAM-FLOW is a Computational Fluid Dynamics (CFD) software product for industrial design activities. It fosters ease of modeling and solution effectiveness by industrial users. PAM-FLOW uses the most recent and advanced numerical and physical modeling techniques such as automatic model generation, adaptive mesh refinement and adaptive remeshing. These, and other features, make PAM-FLOW an ideally suited code for complex transient simulations such as shock wave interactions and coupled fluid-structure interactions including those between moving, deformable bodies. Selected PAM-FLOW Industrial References: France: AEROSPATIALE, MINISTRY OF DEFENSE, RENAULT Italy: ETAS, ENEL, OTO MELARA, Germany: RHEINMETAL Computer Platforms: Supercomputers: Cray, IBM, Convex. UNIX Workstations: SGI, IBM, HP, DEC, SUN. PAM-FLUID is an industrial software simulation tool in support of the design of complex Computational Fluid Dynamic (CFD) Systems. Based on an explicit Finite Element Analysis (FEA) code, it is used for steady state and/or transient, compressible or incompressible viscous flow (Navier-Stokes)simulations. Selected PAM-FLUID Industrial References: Europe: Aerospatiale, GEC Alsthom, OTO MELARA Asia: Mazda, Hino, Daewoo. Computer Platforms: Supercomputers: Cray, IBM, Convex UNIX Work-stations: SGI, IBM, HP, DEC, SUN.
Daat Research Corp.
Daat Research Corp.
P.O. Box 5484
Hanover, NH 03755-5484
Voice: (603)448-1302, 603-643-8145
E-Mail: email@example.comDaat Research has just released CoolitTM, CFD thermal management software for electronic equipment. Coolit provides an integrated Windows NT/95 environment to setup, compute, and analyze electronic packaging designs. Coolit's intuitive graphical interface provides designers with powerful tools previously unavailable in CFD software, such as undo/redo functions and interactive point and click operation. Automatic finite volume grid generation, fast solver which requires only a single parameter to run, and an interactive 3D graphics window for analysis of computed results, make evaluation of 'what if' scenarios easier than ever. Additional information Coolit and Daat Research can be found at http://www.daat.com.
Flomerics Inc. (FLOVENT)
From Peter Schild / Peter.Schild@energy.sintef.no
Date: Mon, 08 Jul 1996 20:42:03 +0200FLOVENT is a special-purpose CFD code for designers of heating, ventilating and air-condirioning systems in buildings and similar structures of all types and sizes. It enables the location and control strategy for HVAC equipment, and the location of smoke detectors, doors, windows, internal partitions, furniture and other obstructions to be optimized for a particular building and its occupants. FLOVENT runs in a windowed environment with drop-down menus, icons and mouse-operated input. It is available on many computer platforms, including PCs. It is both friendly and easy to use. It is also suitable for use as a CFD teaching tool, and is used by a few universities for teaching undergraduate HVAC-engineering students. Developers ---------- FLOVENT has been developed by collaboration between Flomerics Ltd. and the Building Services Research & Information Association (BSRIA) in the UK. Flomerics Ltd. BSRIA The Kingsgate Business Centre Old Bracknell Lane West 12-50 Kingsgate Road Berkshire RG12 7AH Kingston-Upon-Thames England Surrey KT2 5AA Tel: +44-(0)344-426511 England Fax: +44-(0)344-487575 Tel: +44-(0)181-5473373 Fax: +44-(0)181-5472682
Innovative Research, Inc.
Innovative Research, Inc.
2520 Broadway Street NE, Suite 200
Minneapolis, MN 55413
Phone (612) 378-0320 ; Fax (612) 378-0535
firstname.lastname@example.orgWe are a CFD company. We develop general purpose CFD codes and provide consulting services for numerical simulation of heat and mass transfer,fluid flow, and related processes. Our home page address on internet is http://www.inres.com. If you need more information, please feel free to contact us.
Centric Engineering Systems, Inc.
Centric Engineering Systems, Inc.
3393 Octavius Drive, Suite 201
Santa Clara, CA 95054-3004
E-mail: email@example.comProviders of Spectrum Solver and Spectrum Visualizer.
Blue Ridge Numerics, Inc.
Ed Williams or Len Whitehead
Blue Ridge Numerics, Inc.
310 E. Main Street, Suite 300
Charlottesville, VA 22902
Tel: (001) 804-977-2764
Fax: (001) 804-977-2714
E-mail: firstname.lastname@example.orgWe are from a company called Blue Ridge Numerics, Inc. We have been in business for about 4.5 years. We have a finite element based CFD solver that is integrated with COSMOS/M (from Structural Research and Analysis), FEMAP (or NASTRAN for Windows) (from Enterprise Software), I-DEAS Master Series (from Structural Dynamics Research Corp.), and Pro/Engineer (from Parametric Technology). Our web site is www.brni.com.
From David C. Shaw / email@example.com
Organization: NeoSoft, Inc.
WinPipeD is a professional, fully-featured Windows program for analyzing multiphase (oil-gas-water) steady-state pipe flow hydraulics. It utilizes most industry-standard equations and correlations, packaged in an easy-to-use interface. A basic version (b) is available for download for non-commercial use. Production, mechanical, chemical and other engineers involved with fluid mechanics will find this program invaluable. For a trial copy of the program, or a Windows help file with its complete documentation, please send e-mail to: firstname.lastname@example.org and they will be sent by return e-mail. Please visit our site at: http://www.neosoft.com/~dshaw/winpiped.html for more details.
From Steve Weinberger / email@example.com
Date: Tue, 21 Jan 1997 17:03:35 -0500
Exa Corporation website (www.exa.com) can provide alot of the information also on PowerFLOW product.
From Yves RUBIN / firstname.lastname@example.org
Date: Mon, 17 Feb 1997 09:55:25 +0100
16, Place de l'Universite
Technical Director : Dr. J-M. Marchal
Customer Support Manager : Mr. B. Hocq
Business Manager: Mr. Y. Rubin
Product Manager: Mr. T. MarchalThe Polyflow s.a. company - Polyflow S.A. is located in Louvain-la-Neuve in Belgium and has sales and technical support offices in the USA, Japan, Korea Taiwan, the Czech Republic and Israel. The company, founded in 1988, accelerates technology transfer through research and development of new software capabilities and cooperates with universities and research groups to remain at the forefront of technology in the area of flow modelization and advanced numerical methods. It provides industrial technical centers and research and development laboratories with the latest progresses in finite element simulation methods in a user-friendly environment. Polyflow is the leader in simulations of the processing of complex materials in industrial flows and is resolutely oriented towards the industrial applications and the design and understanding of processes where viscous flows play a major role under isothermal and non-isothermal conditions, such as flow of plastic, rubber, glass or food stuff. To date, POLYFLOW licenses have been acquired by more than 155 companies and academic centers throughout the world, distributed between Europe, North America and Asia (Japan and Korea mainly), where Polyflow has a leading position in the field of computer aided processing in the plastics and chemical industry. A group of Ph.D. and highly skilled engineers provide consulting and maintenance activities to all users and customers. They don't hesitate to travel and to visit customers in order to establish a relationship based on confidence and user satisfaction. Product names: The main product is the POLYFLOW package, which comprises its own mesh generators, parameters input module, the solver and graphical post-processor. Several modules are available for the solver such as the Viscoelastic or Blow Molding simulation capabilities and for interfaces with existing pre- and post-processors, such as Patran, I-Deas and more. Third-party products such as the Polycem CAD/mesh generator product and the CFView-PF graphical post-processor are also available with POLYFLOW. Platforms: The POLYFLOW package runs on most platforms, from Unix workstations (Silicon Graphics, IBM, Hewlett-Packard, Sun, DEC), up to major supercomputers, such as Convex or Cray computers. Presentation of the company's activities and strategic vision The POLYFLOW product is international by nature and distributed worldwide to major plastics, rubber and resins producers, glass industries and plastics and rubber transformers in the fields of construction (e.g. window profiles), automotive industry and consumer goods (e.g. rubber profiles, gas tanks, seals, bottles with handles) and medical supplies (e.g. catheters), among others. The market for POLYFLOW is distributed almost evenly between Europe, where Polyflow S.A. markets its product, North America (through a distrbutor) and Asia (also through distrbutors, mainly in Japan, Korea and Taiwan), and new markets begin to emerge such as Australia and China. Among the typical customers of POLYFLOW thus far are companies like Daikin, Solvay, Glaverbel, Dow, General Electric, Allied-Signal, Owens-Corning =46iberglass, Sumitomo, Mitsubishi Chemical, the tire industry, to name a few. For its work in the numerical modelling of fluids in industrial flows to provide a tool for a better understanding of the physics of the process and the optimization of the geometry and operational conditions, Polyflow S.A. has been awarded in 1990 the Gold Prize for Technological Innovation granted by the Walloon Region. POLYFLOW is already sold in large industrial groups on the three main geographical areas, and the company plans to reinforce its activities in the field of consulting for smaller size companies who do not wish to maintain permanently a study group but would certainly benefit from the numerical simulation capabilities offered by POLYFLOW and its experienced team of engineers, without having to invest in the acquisition of the program or initial training in this technology. In this way, Polyflow S.A. will be able to make POLYFLOW simulation available to a larger number of companies and providing an answer to day-to-day industrial problems, especially in the extrusion and blow molding processes and for flows in the confined domains of extrusion equipment. The goal of the Polyflow company is also to solve industrial problems, participate in a larger acceptation of Computer Aided Processing in the industry and highlight the important savings for industries through the reduction of costly trial and error procedure; these savings may come from less manufacturing and testing of new dies, the reduction of idle time for the production line and wasted material, which is often not (easily, if at all) recyclable, another ecological aspect more widely accepted nowadays than ever before.
From Rick Palmer / email@example.com
Date: Tue, 18 Feb 1997 08:33:41 -0800Flow Pro is a steady-state open channel water surface profile program for hydraulic engineers. Flow Pro uses Manning's equation and numerical integration to compute depth, velocity, energy, momentum, and area of flow for subcritical and supercritical open channel flow. Flow Pro supports trapezoidal, circular, ushaped, and tubular channel shapes. Flow Pro was developed by ProSoft Apps with versions for Windows 3.1 and Windows 95/NT. ProSoft Apps can be found on the Internet at http://www.europa.com/~psapps/ and can be contacted via email at firstname.lastname@example.org. Flow Pro 2.0 is a Windows hydraulic analysis package for open channels, weirs, orifices, and underflow gates. Please visit us online for program details, and to download a free fully functional demo. Please direct any inquiries to Rick Palmer at email@example.com
Computational Aerodynamics Systems Co.
Computational Aerodynamics Systems Co.
Tel/fax : +7 095 176-18-34
Tel : +7 095 158-40-74
e-mail : firstname.lastname@example.orgAeroShape-3D General possibilities : Steady or transient; Inertial or non-inertial frames of reference; volumetric sources (mass, heat, chemical species, etc.); Moving bodies (walls); objects of variable geometry, free surface motion, K-E or RSM turbulence model with corrections for wall conditions (heat fluxes and friction); Combustion models, equilibrium or non-equilibrium chemical reactions; Two phase flows; media with special state equation; Non-compressible, sub-, trans- and supersonic flows , hypersonic flows. Carefully tested and validated on diverse industrial problems (aerospace, automotive, power, HVAC, artificial organs, etc.). A lot of educational applications. The core of AeroShape-3D is based on finite volume Rectangular Adaptive Mesh (RAM) technique for complex 3D flow simulation. The main advantage of RAM technique is very high accuracy together with unique flexibility in adaptation to complex 3D geometry of body and flow structure and simultaneous efficiency in computer resources use. Hardware: IBM PC (Windows'95 or NT) or Work Station (X-Windows, UNIX). RAM > 24Mb and HDD > 50Mb Contact person: A. Sobatchkine
Tahoe Design Software
From Brian Haulman / email@example.com
We commercially develop software for fluid conveyance system modeling. Our URL is: http://www.tahoesoft.com.
PO Box 8128
Truckee, CA 96162
ADINA-F, a CFD solver of the ADINA System, is based on finite element and finite volume discretization schemes. General incompressible or compressible flow conditions with or without heat transfer in arbitrary geometries can be solved. The flow may contain free surfaces and moving interfaces between fluids. Multi-physics fluid flows with structural interaction capabilities allows to solve complex coupled problems.
The ADINA Analysis System has the following modules:
http://www.mrl.itri.org.tw/yflow/yflow.htm (in Chinese Big5)
http://www.mrl.itri.org.tw/yflow/english.htm (in English)
YFLOW is a general purposed transient analysis finite element code on fluid dynamics with special capability for sliding mesh and deformable mesh. Several CFD results with animation and VRML are shown (for examples: air floating dryer, cross flow fan, centrifugal pump...).
Date: Sun, 20 Jul 1997 11:34:31 -0400 From: Peter GarrisonI want to call your attention to a commercial CFD package. It is PSW (formerly Personal Skunk Works, now, thanks to Lockheed, Personal Simulation Works), created by AeroLogic in Los Angeles. It includes a meshing preprocessor, an improved version of Pmarc-12, and a powerful graphic postprocessor. Our web page is
Subject: another CFD product
Note that that's AEROL, not AERO1.
Advanced Visual Systems, Inc.
300 5th Avenue
Waltham, MA 01254
Visualization software systems AVS, AVS/Express, Gsharp, Toolmaster, provide both end-user visualization programs for CFD post-processing, and development systems and libraries that are used to create new custom applications. Application design and prototyping uses supplied components or user-written components, assembled in a visual network editor.
AVS CFD visualization facilities include slice, cut, crop, isosurface, isovolume, line contours, solid contours, streamlines, stream ribbons, vector glyphs, particle animation, transient data animation, dynamic mesh rezoning, camera & light source movement, and output to postscript, VRML, MPEG, TIFF, GIF, JPEG, etc. Data structure support includes 2D/3D structured grids, multi-block grids, and fully unstructured meshes.
File import facilities include NetCDF, PLOT3D, FIDAP, Fluent/UNS, Rampant, STAR-CD, CFX, Phoenics, Autodyn, LS-Dyna3d, MSC-Dytran, and others.
Information contributed by Ian Curington ( firstname.lastname@example.org ) August 1997
Product: Flo++ Developed by: Softflo 11 Drommedaris Str. Potchefstroom, 2531 South Africa Contact info: http://www.softflo.com Email: email@example.com Fax: (+27) 148 297 0061 Phone: (+27) 148 297 0029
Availability: Flo++ is a commercial code. A free, fully functional but limited cell evaluation copy can be downloaded from our web site.
Description: Flo++ Computational Flow Dynamics Software for Windows NT & Windows 95
Flo++ is a general-purpose, finite volume, PC based computational fluid dynamics program for the solution of industrial fluid flow and heat transfer problems.
Flo++: Runs on a PC under Windows 95 or Windows NT or a DEC Alpha under Windows NT; Has an intuitive, Windows graphical user interface; Contains Windows Help facilities offering support at your fingertips; Caters for a wide range of fluid flow capabilities; Caters for complex geometries; Makes provision for user coding in C/C++ to define complex source terms or property definitions.
More information, examples and a free download are available from our web site: http://www.softflo.com
K S N I S iterative solver for sparse NONSYMMETRIC INDEFINITE systems of equations using preconditioned Krylov subspace iterative methods. It has special options for SYMMETRIC INDEFINITE and SYMMETRIC POSITIVE DEFINITE systems. INPUT DATA ---------- 1) General nonsymmetric case: -- N - problem size, -- COA(1:LENG) real*8 array for compactly stored matrix in the row-by-row manner, -- JCOA(1:LENG) integer array such that JCOA(k) = Collumn Number of matrix entry COA(k), -- BEGA(1:N+1) integer array of pointers to first entries in rows of the compactly stored matrix, LENG=BEGA(N+1)-1, -- DIA(1:N) integer array of pointers to diagonal entries in rows of the compactly stored matrix, -- RHS(1:N) real*8 array for the right-hand side vector. EXAMPLE: 1 0 2 0 Matrix 3 4 0 5 0 6 7 0 0 8 0 9 COA: 1 2 3 4 5 6 7 8 9 (LENG=9) JCOA: 1 3 1 2 4 2 3 2 4 BEGA: 1 3 6 8 10 DIA: 1 4 7 9 2) Symmetric case: -- N - problem size, -- COA(1:LENGSYM) real*8 array for compactly stored column-by-column the upper part of the matrix, -- JCOA(1:LENGSYM) integer array such that JCOA(k)=Row Number of matrix entry COA(k), -- BEGA(1:N+1) integer array of pointers to first (diagonal) entries in columns of the compactly stored matrix, LENGSYM=BEGA(N+1)-1, EXAMPLE: 1 0 4 0 Matrix 0 2 0 6 4 0 3 0 0 6 0 5 COA: 1 2 3 4 5 6 (LENG=6) JCOA: 1 2 3 1 4 2 BEGA: 1 2 3 5 7 In case of symmetric positive definite system typical storage requirements correspond to storing two symmetric parts including the diagonal (2*LENGSYM) and several work arrays of size N. In case of symmetric indefinite system typical storage requirements correspond to storing one symmetric part including the diagonal (LENGSYM), entire compactly stored sparse matrix (LENG) and several work arrays of size N. In case of nonsymmetric system typical storage requirements correspond to storing two entire compactly stored sparse matrices (2*LENG) and several work arrays of size N. ITERATIVE EQUATION SOLVER K S N I S DEMONSTRATED GOOD PERFORMANCE IN MANY LARGE-SCALE FINITE ELEMENT, FINITE DIFFERENCE AND CONTROL VOLUME LINEAR AND NONLINEAR ANALYSES OF UNSTEADY CONVECTION-DIFFUSION, COUPLED GEOMECHANICS, THIN SHELLS NEAR BUCKLING, SOLIDS, FRAME AND TRUSS STRUCTURES, HEAT CONDUCTION AND OTHER APPLICATIONS. The solver can be easily used through the interface file as well as incorporated into the FE code. Fortran-77 and C versions of the solver are available. ----------------------------------------- Contact address: Prof. Vitaly Bulgakov, Dept. of Applied Mathematics, Moscow State University of Civil Engineering, 129337 Moscow, Yaroslavskoe Shosse 26 R U S S I A tel. +7 (095) 183-59-94/282-80-00 E-mail: firstname.lastname@example.org email@example.com
Company: Flowcode Ltd. Address: 20 Meadway Close Staines Surrey TW18 2PR United Kingdom Telephone: +44 (0) 1784 464 911 Fax: +44 (0) 1784 464 711 E-Mail firstname.lastname@example.org Web Site http://www.flowcode.com Flowcode is developing a computational fluid dynamics package for the analysis of hydro/aerodynamics. The code uses a time-stepping approach to allow unsteady problems to be analysed. Please note that the code is still under development and is not yet commercially available. Our website includes details about Flowcode, a summary of the applications and technology used, links to relevant sites and a feedback form to register for more information.
Code: ConcertConcert is a CFD software for analysing fluid flow, heat transfer, and other coupled physical phenomena. It has object-based modules for most tasks associated with CFD, e.g.
Company: Numeritec Corporation
Address: 427 Amherst Street, Suite 11
Nashua, NH 03063
Phone: (603) 889-2800
FAX: (603) 889-2882
John A. C. Ewer School of Maths, University of Greenwich, Wellington Street, Woolwich, London, SE18 6PF, United Kingdom. (+44) (Work)0181-331-8658 (Fax)0181-331-8665 (Mobile)0958-330-665 email@example.com http://www.gre.ac.uk/~ej02
SMARTFIRE has been developed by the Fire Safety Engineering Group at the University of Greenwich (UK) as part of an EPSRC funded project.
The software has been used on short courses in fire modelling given by the University of Greenwich and the software is now being made available commercially for anyone involved in fire field modelling. The initial release is for PC's running windows 95 and windows NT 4.0 but the port to motif based Unix boxes is due shortly.
SMARTFIRE is an interactive fire field modelling CFD code that incorporates knowledge based techniques to assist in the specification of simulations. The software also has integral run-time control, monitoring and visualisation capabilities built into the unstructured mesh CFD engine. The numerical engine is based on the SIMPLE algorithm with coupled Flow, K-e model turbulence, Enthalpy and Six flux radiation.
More information about the software can be obtained from our web site at:
or by Emailing
Airflow Sciences Corporation
Main Office:(734) 464-8900
37501 Schoolcraft Rd.
VISCOUS is a control volume based CFD code capable of modeling a general flow field simulation. Problems may be 2D or 3D, steady state or time dependent, and laminar or turbulent. Conjugate heat transfer and the convection/diffusion of an arbitrary number of field variables may be modeled. Additional modules to handle radiation, combustion and a variety of other phenomena are available.
Over the past ten years, VISCOUS has been used to solve problems in a wide variety of fields including power generation, transportation, food technology and manufacturing.
Here's another entry to your list. A company called Polydynamics (based in Hamilton, Ontario, Canada) has a commercially available software package called Polycad, which incorporates modules for the simulation of different polymer processing operations, using finite element based codes. Here's the link:
---------------------------------------------------------------------------- David Strutt firstname.lastname@example.org UWaterloo chem eng grad student email@example.com (519) 885-1211 ext. 3816 Homepage: http://cape.uwaterloo.ca/~dstrutt/
From Brent Cullimore / firstname.lastname@example.org
Cullimore and Ring Technologies, Inc.
9 Red Fox Lane
Littleton Colorado 80127-5710
C&R Technologies offers the world's most powerful general purpose thermal/hydraulic analyzer, SINDA/FLUINT, plus a dedicated nongeometric (circuit sketchpad) GUI, SinapsPlus(tm). Also available for thermal engineers is a geometric (CAD/FDM/FEM) interface, Thermal Desktop(tm), plus a fast radiation analyzer, RadCAD(R).
A comprehensive finite-difference lumped-parameter tool for analyzing complex thermal/fluid systems. Suitable for both preliminary design and point design simulation, at both the component and system level. SINDA/FLUINT is used at over 400 sites in the aerospace, energy, electronic, HVAC, medical, and automotive industries.
Capabilities include: steady and transient analyses, radiation, convection, and conduction heat transfer, single- and two-phase flow, fluid mixtures, time- and temperature-varying properties, and user logic for control and customization. A built-in spreadsheed allows rapid parametric model changes. Also featured are a design optimizer and data correlator.
Applications include thermal and environmental control, propulsion, electronics packaging, and power generation.
A modern graphical user interface to SINDA/FLUINT. Enables users to sketch thermal/fluid circuits, validate/preprocess inputs interactively, and then visualize, interpret, and report results graphically.
Capabilities include: algebraic and functional in-puts; depiction of large, complex networks, colorization by value, animation through time, and pop-up X-Y, bar, and polar plots.
PC (Windows 95/98/NT)
Sun (Solaris 2.X)
The site contains product information, brochures, tutorials, class notes, complete user's manuals, and free evaluation versions which solve small problems. Also available free are fin (extended surface) and 1- or 2-phase pipeflow modeling tools as part of the SinapsPlus package.
PLEASE TAKE NOTE OF THE LICENSE AGREEMENT AND SYSTEM REQUIREMENTS BEFORE DOWN- LOADING OR INSTALLING THESE CODES. SINDA/FLUINT requires a specific Fortran 77 compiler on each machine (which regrettably are not ours to offer for free).
ANKER - ZEMER ENGINEERING A/S
Tel: +47-22 13 95 80
Fax: +47-22 13 95 95
Web address: www.anker-zemer.com
email address: DT.ZEMER@ANKER-ZEMER.NO
The BEM (Boundary Element Method) program LINFLOW is a newly developed program for linear steady and unsteady fluid flow calculations in 3D. Since all structures are described by surfaces only, the analysis time when solving problems using LINFLOW is reduced to only a few percent of the time required by standard software using the full Navier-Stokes equations.
Performance Fluid Dynamics (PFD) Limited
40 Lower Leeson Street
Dublin 2 / Ireland
tel : +353 1 66 121 31
fax : +353 1 66 121 32
E-mail : email@example.com
PFDReaction : an add-on to general purpose CFD programs enabling chemical kinetics to be included correctly in turbulent flow simulations.
Airfoil Analysis is a professional-level airfoil analysis system package for the Microsoft Windows 95, 98 and Windows NT environment. It is developed for use by anyone who needs fast, accurate wing airfoil analysis and wants the power and flexibility afforded by Windows95/98/NT.
COMET is multi-purpose CCM-Software for the solution of continuum mechanics problems (both fluid and solid mechanics). It is a self-contained package incorporating mathematical models of a wide range of thermo-fluids and solids phenomena, powerful solvers enabling full complex-geometry capabilities, highly efficient and stable set of numerical solution algorithms, flexible pre-processing and post-processing facilities tailored for both expert and novice users.
COMET is developed by professionals who have been at the forefront of both the research and the commercial software development in the field of computational continuum mechanics in the last 15 years. The code is based on the authors' own pioneering work in the fields of discretisation by arbitrary (moving) meshes, error detection, full multigrid acceleration techniques, parallel computing and finite volume stress analysis.
CFD++ is a thoroughly modern general purpose Computational Fluid
Dynamics software for accurate and efficient flow simulations. Its
unified-grid, unified-physics and unified-computing methodology
applies to ALL flow regimes, ALL types of mesh and cell topologies,
and ALL computing platforms and offers exceptional effectiveness and
value. Let CFD++ and
Metacomp Technologies help you achieve the most
out of CFD technology.
The RADIOSS-CFD system includes several modules: -M-Explicit is a compressible, coupled fluid structure, explicit solver. The main use of tis module is aeroacoustic simulations of automotive components (Intakes, Exhausts, Air conditionning, fans) and also full vehicle models. It is used worldwide by clients like Ford, Toyota, Case, ... -M-Implicit is an incompressible implicit Navier Stokes solver. This module brings unprecedented robustness and accuracy in the implicit solvers domain thanks to the use of Galerkin/Least-Squares algorithms and a proprietary algebraic solver addressing the coupled pressure-velocity system as a whole.
Since its first use in industry more than 10 years ago and its commercial release in 1994, VECTIS has gained widespread acceptance in the powertrain industry as highly versatile and efficient software for finite-volume CFD analysis. VECTIS features a range of engine-specific physical models which are subject to rigorous application-focused validation, together with high levels of integration with CAD and other CAE systems. It also features a unique, fully automatic mesh generation technology capable of providing a mesh accurately conforming to virtually any flow domain geometry.