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Computational Mechan
Austin, TX, 78757 0102
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HUBZone Owned: N
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Award Charts
Award Listing
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SBIR PHASE I: The Mathematical Theory and Implementation ofh-p Adaptive Meshless Analysis for Interdisciplinary Applications and High-Performance Computing
Amount: $300,000.00N/A
SBIRPhase II1998National Science Foundation -
Hp-Meshless Cloud Method for Dynamic Fracture in Fluid Structure Interaction
Amount: $200,000.00COMCO proposes to develop a new, meshless computational methodology for dynamic fracture simulation in fluid-structural interaction. Our approach is based on a new class of methods which eliminate al ...
SBIRPhase II1996Department of Defense Navy -
SBIR PHASE I: The Mathematical Theory and Implementation ofh-p Adaptive Meshless Analysis for Interdisciplinary Applications and High-Performance Computing
Amount: $75,000.00N/A
SBIRPhase I1996National Science Foundation -
Hp-Meshless Cloud Method for Dynamic Fracture in Fluid Structure Interaction
Amount: $70,000.00N/A
SBIRPhase I1995Department of Defense Navy -
Dynamic Load Balancing for Distributed Finite Element Analysis
Amount: $65,000.00N/A
SBIRPhase I1995National Science Foundation -
DISTRIBUTED-NETWORK PARALLEL COMPUTING FOR ADAPTIVE METHODOLOGIES IN COMPUTATIONAL FLUID DYNAMICS
Amount: $50,000.00A GENERAL-PURPOSE, SOLUTION-ADAPTIVE, FINITE-ELEMENTS CODE THAT TREATS BROAD CLASSES OF INCOMPRESSIBLE FLOWS HAS BEEN DEVELOPED. THE CODE EMPLOYS H-ADAPTIVE AND P-ENRICHMENT ALGORITHMS THAT REFINE THE ...
SBIRPhase I1992Department of Energy -
A FINITE ELEMENT CFD CODE FOR GENERIC GUN BORE EVACUATOR AND FLAREBACK CONTROL
Amount: $525,000.00N/A
SBIRPhase II1992Department of Defense Army -
HIGHLY ACCURATE ADAPTIVE TECHNIQUES FOR DAMAGE MODELING & LIFE PREDICTION OF AEROSPACE STRUCTURES
Amount: $49,946.00N/A
SBIRPhase I1992National Aeronautics and Space Administration -
ADVANCED ADAPTIVE COMPUTATIONAL METHODS FOR NAVIER-STOKES SIMULATIONS IN ROTORCRAFT AERODYNAMICS
Amount: $500,000.00A 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 ...
SBIRPhase II1990Department of Defense Army -
A NEW APPROACH FOR SOLVING NAVIER-STOKES EQUATIONS ON UNSTRUCTURED GRIDS BASED ON ADAPTIVE METHODS AND OPERATOR-SPLITTING
Amount: $529,291.00TODAY AN OVERWHELMING MAJORITY OF CFD CALCULATIONS ARE DONE WITH STANDARD FIXED GRID FINITE DIFFERENCE METHODS. HOWEVER, A SIMPLE CALCULATION CAN ESTABLISH THAT SUCH METHODS CANNOT POSSIBLY EXPLOIT TH ...
SBIRPhase II1990National Aeronautics and Space Administration
