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AEROSOFT INC
UEI: ZCHKAN7GL6N1
# of Employees: 5
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Multi-Variable Sensitivity Technology for Enhancing Future Aircraft
Amount: $98,855.00Recent advancements in both computational efficiency and physical-modeling capabilities have increased the utility of computational fluid dynamics in the vehicle-design process. However, beyond knowi ...
SBIRPhase I1998Department of Defense Air Force -
An Efficient, Unstructured Flow Solver for Complex Aircraft Configurations in Maneuvering Flight
Amount: $642,351.00AeroSoft proposes the development of efficient and accurate Computational Fluid Dynamics methods for calculating the airflow characteristics over complex bodies with time-dependent, Reynolds-Ave ...
SBIRPhase II1997Department of Defense Air Force -
Modeling Laminar to Turbulent transistion for improved high lift predictions
Amount: $68,433.00AeroSoft, Inc. proposes to develop, incorporate and validate transition and anisotropic turbulence models for improving the low-Reynolds number predictions for high-lift airfoil configurations. The t ...
SBIRPhase I1997Department of Defense Navy -
A Stand-Alone Sensitivity Solver For Hypersonic Design Applications
Amount: $66,432.00N/A
SBIRPhase I1997National Aeronautics and Space Administration -
Time-Accurate Simulatiion of Moving Bodies Using Unstructured Technology
Amount: $746,266.00A robust and accurate extension of an existing state-of-the-art steady-state compressible unstructured flow solver and grid generation package to include time-accurate simulation of multiple moving bo ...
SBIRPhase II1996Department of Defense Navy -
An Efficient, Unstructured Flow Solver for Complex Aircraft Configurations in Maneuvering Flight
Amount: $99,764.00N/A
SBIRPhase I1996Department of Defense Air Force -
An Unstructured Gasp Flow Solver For Use In The Design Of Liquid And Solid Rocket Engines
Amount: $69,510.00N/A
SBIRPhase I1995National Aeronautics and Space Administration -
An Efficient, Unstructured Flow Solver For Space-Physics Applications
Amount: $69,661.00N/A
SBIRPhase I1995National Aeronautics and Space Administration -
Economical Aero-Propulsion Shape Optimization For Hypersonic Design Applications
Amount: $69,896.00N/A
SBIRPhase I1995National Aeronautics and Space Administration -
INCORPORATION OF ARBITRARY GRID PATCHING INTO GASP VERSION 3.0
Amount: $197,229.00The objective of this Phase I research is to implement a conservative method for transferring data across arbitrary nonoverlapping zonal interfaces in the CFD code GASP version 3.0. This task will inv ...
SBIRPhase II1994Department of Defense Air Force
