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Computational Mechan

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Address
7800 Shoal Creek
Austin, TX 78757 0102
United States
Information

UEI: N/A

# of Employees: N/A
Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No

Award Charts




Award Listing

  • Record 1 TO 31

  1. PRE- AND POST-PROCESSING TECHNIQUES FOR DETERMINING "GOODNESS" OF COMPUTATIONAL MESHES.

    Amount: $497,444.00

    IN CONTEMPORARY COMPUTATIONAL FLUID DYNAMICS, FINITE DIFFERENCE OR FINITE ELEMENT GRIDS ARE OFTEN GENERATED USINGSTANDARD MESH GENERATION TECHNIQUES. THE BETTER MESH GENERATION PACKAGES ARE CAPABLE OF ...

    SBIRPhase II1990National Aeronautics and Space Administration

  2. HIGHLY ACCURATE SKIN FRICTION AND HEATING RATE PREDICTIONS USING NOVEL ADAPTIVE TECHNIQUES

    Amount: $49,968.00

    ACCURATE AND EFFICIENT PREDICTION OF SKIN FICTION AND HEATING RATES FOR SUPERAND HYPERSONIC VEHICLES HAS LONG BEEN A GOAL OF COMPUTATIONAL FLUID DYNAMICS (CFD). THE USE OF STANDARD CFD METHODS TO RESO ...

    SBIRPhase I1990Department of Defense Air Force

  3. A FINITE ELEMENT CFD CODE FOR GENERIC GUN BORE EVACUATOR AND FLAREBACK CONTROL

    Amount: $50,000.00

    N/A

    SBIRPhase I1990Department of Defense Army

  4. A COMPREHENSIVE PNS UPGRADE FOR THREE-DIMENSIONAL REENTRY FLOW PREDICTION

    Amount: $650,000.00

    THE MISSION OF THIS PHASE I PROJECT IS COMPLETION OF A TRULY INNOVATIVE STUDY TO UPGRADE EXISTING PNS CODES FOR COMPUTING HIGHSPEED, THREE-DIMENSIONAL RE-ENTRY FLOWFIELDS. THE PLAN OF ACTION ENCOMPASS ...

    SBIRPhase II1989Department of Defense Air Force

  5. ADAPTIVE SCHEMES FOR COMPLEX SUBSONIC 3D-FLOW PROBLEMS IN ARBITRARY DOMAINS

    Amount: $489,099.00

    THIS PROJECT IS DEVOTED TO THE DEVELOPMENT OF A UNIQUE COLLECTION OF ALGORITHMS DESIGNED TO RESOLVE SOME OF THE MOST DIFFICULT PROBLEMS OF MODERN COMPUTATIONAL FLUID DYNAMICS: (1) THE ANALYSIS OF COMP ...

    SBIRPhase II1989National Aeronautics and Space Administration

  6. PRE- AND POST-PROCESSING TECHNIQUES FOR DETERMINING "GOODNESS" OF COMPUTATIONAL MESHES.

    Amount: $50,000.00

    N/A

    SBIRPhase I1989National Aeronautics and Space Administration

  7. A NEW APPROACH FOR SOLVING NAVIER-STOKES EQUATIONS ON UNSTRUCTURED GRIDS BASED ON ADAPTIVE METHODS AND OPERATOR-SPLITTING

    Amount: $50,000.00

    N/A

    SBIRPhase I1989National Aeronautics and Space Administration

  8. ADVANCED ADAPTIVE COMPUTATIONAL METHODS FOR NAVIER-STOKES SIMULATIONS IN ROTORCRAFT AERODYNAMICS

    Amount: $50,000.00

    N/A

    SBIRPhase I1988Department of Defense Army

  9. ADAPTIVE SCHEMES FOR COMPLEX SUBSONIC 3D-FLOW PROBLEMS IN ARBITRARY DOMAINS

    Amount: $47,000.00

    N/A

    SBIRPhase I1988National Aeronautics and Space Administration

  10. AN ARBITRARY GRID CFD ALGORITHM FOR CONFIGURATION AERODYNAMICS

    Amount: $200,000.00

    THIS PROPOSAL DESCRIBES A PROJECT TO DEVELOP AND EXAMINE A CFD NUMERICAL SOLUTION ALGORITHM FOR THE THREE-DIMENSIONAL EULER/NAVIER-STOKES EQUATIONS THAT DOES NOT RELY ON A WELL-STRUCTURED, BODY-FITTED ...

    SBIRPhase II1987National Aeronautics and Space Administration
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