Computational Mechan

Company Information

Company Name
Computational Mechan
Address
7800 Shoal Creek
Austin, TX, 78757 0102
Phone
n/a
URL
n/a
DUNS
n/a
Number of Employees
n/a
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,006,121.00
19
SBIR Phase II
$5,081,834.00
12
Chart code to be here

Award List

  1. THE CURRENT STATE OF ROBOTIC TECHNOLOGY IS FAR FROM THE GOALOF AUTOMATED INTELLIGENT BEINGS.

    Amount: $49,708.00

    THE CURRENT STATE OF ROBOTIC TECHNOLOGY IS FAR FROM THE GOALOF AUTOMATED INTELLIGENT BEINGS. IN THE INDUSTRIAL SCENARIO WHERE MUCH OF THE CURRENT ROBOT DEVELOPMENT HAS BEEN APPLIEDMOST ROBOTS ARE LITT ...

    SBIR Phase I 1983 ArmyDepartment of Defense
  2. AUTOMATED AMMUNITION LOADING OF COMBAT VEHICLE

    Amount: $500,000.00

    THE CURRENT STATE OF ROBOTIC TECHNOLOGY IS FAR FROM THE GOAL OF AUTOMATED INTELLIGENT BEING. IN THE INDUSTRIAL SCENARIO WHERE MUCH OF THE CURRENT CURRENT ROBOT DEVELOPMENTHAS BEEN APPLIED, MOST ROBOTS ...

    SBIR Phase II 1984 ArmyDepartment of Defense
  3. HYERSONIC AIR-BREATHING ENGINE INLET ANALYSIS

    Amount: $49,859.00

    THIS PROPOSAL DDESCRIBES AN SBIR PROJECT TO ESTABLISH AN IMPROVED ANALYITCAL TECHNIQUE IN EXTERNAL AND \ OR INTERNALLY DUCTED FLOW PROPERTIES FOR HYPERSONIC ENGINE AIR LINLETS. THE GOAL OF THIS PHASE ...

    SBIR Phase I 1983 NavyDepartment of Defense
  4. 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 ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  5. ADAPTIVE COMPUTATIONAL METHOD FOR FLUID-STRUCTURE INTERACTION IN INTERNAL FLOWS

    Amount: $491,000.00

    SUPER ACCURATE ADAPTIVE COMPUTATIONAL SCHEMES FOR THE ANALYSIS OF FLUID STRUCTURE INTERACTION AND COMPLEX THREE-DIMENSIONAL INTERNAL FLOWS ARE TO BE DEVELOPED. NEW PETROV-GALERKIN FINITE ELEMENT METHO ...

    SBIR Phase II 1987 National Aeronautics and Space Administration
  6. ADAPTIVE GRID TECHNIQUES FOR USE IN COMPUTATIONAL FLUID DYNAMICS

    Amount: $200,000.00

    THIS PROJECT FOCUSES ON THE TWO MOST IMPORTANT ISSUES OF ALL OF COMPUTATIONAL FLUID DYNAMICS: 1) HOW GOOD ARE THE NUMERICAL ANSWERS OBTAINED IN A COMPUTATION? AND 2) HOW CAN THE BEST POSSIBLE ANSWERS ...

    SBIR Phase II 1987 Air ForceDepartment of Defense
  7. 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 ...

    SBIR Phase II 1989 Air ForceDepartment of Defense
  8. A ROBUST UNSTEADY INCOMPRESSIBLE NAVIER STOKES CODE

    Amount: $50,000.00

    THE MISSION OF THIS PHASE I PROJECT IS TO DEVELOP A ROBUST AND ACCURATE COMPUTER CODE FOR PREDICTING INCOMPRESSIBLE TRANSIENT TURBULENT FLOWFIELDS USING AN INTEGRAL (FINITE VOLUME) TECHNIQUE. THE CODE ...

    SBIR Phase I 1987 NavyDepartment of Defense
  9. 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 ...

    SBIR Phase II 1989 National Aeronautics and Space Administration
  10. ADVANCED ADAPTIVE COMPUTATIONAL METHODS FOR NAVIER-STOKES SIMULATIONS IN ROTORCRAFT AERODYNAMICS

    Amount: $500,000.00

    A NEW AND INNOVATIVE CLASS OF ADAPTIVE COMPUTATIONAL PROCEDURES IS TO BE DEVELOPED FOR THE SPECIFIC PURPOSE OF NUMERICALLY-MODELING COMPLEX FLOWS INHERENT IN ADVANCED HELICOPTER-BLADE DESIGNS. THESE P ...

    SBIR Phase II 1990 ArmyDepartment of Defense

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