- Aerospatiale, Paris, France.
CFD analysis of a turbo-reactor
- ACRi France, Sophia Antipolis, France.
CFD Design of the new Beijing Opera House Building"s HVAC System.
- IDOM, Bilbao, Spain.
CFD analysis of wind loads on an architectural "canopy", part of the new Guggenheim Museum in Bilbao, Spain.
- IDOM, Bilbao, Spain.
Simulation of a mandrel used in manufacturing of gas turbine blades' composite components
- Allison Gas Turbine, Indianapolis, IN.
Development of ANSWER software for combustor design methodology
- Allison Gas Turbine, Indianapolis, IN.
Development of an efficient Reynolds stress model for combustor applications
- Brown Boveri-Sulzer Turbomachinery Ltd., Switzerland.
Blade with transpiration, film-cooling and transition
- C.N.I.M., Toulon, France.
Design and analysis of submarine hull and components
- ENEL,Italy & Caltech,Pasadena,CA
Stability analysis of a Westinghouse-Mitsubishi powergen GT Combustor
- Garrett Turbine Engine Company, Phoenix, AZ.
Development of a stochastic random-walk algorithm, for spray combustion
- GE Aircraft Engines, Cincinnati, OH
Support services for in-house CFD and combustion analysis
- GE Aircraft Engines, Cincinnati, OH
Development of the Advanced Combustion Code (ACC) from the ACRi ANSWER to replace the in-house CONCERT code
- GE Aircraft Engines, Cincinnati, OH
Development of a general purpose combustion dynamics tool (ACD)
- GE Aircraft Engines, Cincinnati, OH
Development of a Finite-rate chemisty Monte-Carlo Stirred-Reactor Model to predict combustor emissions, ignition and blowout
- GERPY-DECAN, Toulon, France.
CFD analysis for optimization and design of torpedo launch tubes
- Hyperspace, Paris, France.
Consulting and review of CFD and combustion for a hypersonic vehicle
- Marquardt Corporation, Van Nuys, CA.
Development and testing of low L/D, high swirl ramjet concepts
- NASA, Ames, CA
CFD & Acoustic coupling for jet noise (with Northrop & UCLA)
- NASA, Cleveland, Ohio
Simulation of flames in modified gravity environments
- NASA, Cleveland, Ohio
HOST Program: Development of Improved Numerical Methods
- NASA, Cleveland, Ohio
AST Program; design & performance analysis
- NASA, Cleveland, Ohio
NCC Program: Development of Turbulence & Radiation Modules for NCC
- NASA, Cleveland, Ohio
HSCT Program: Performance and design analysis
- Northrop,CA & UCLA, CA
Coupled CFD & Acoustic simulations with LES for Jet noise prediction
- Rolls-Royce (BED) Ltd., England.
Combustion in ducts. RB99 Afterburner analysis
- SNECMA, Villaroche, Paris, France.
Development of ECRIN 3-D; derived from ACRi ANSWER
- SNECMA, Villaroche, Paris, France.
Testing of ECRIN with laboratory and field data for engine performance
- SNECMA, Villaroche, Paris, France.
Modification of COM-3-D code to incorporate advanced turbulence models, NOx emissions model and improvements in the I/O interface.
- Turbomeca, Paris, France.
Support for in-house CFD applications
- U.S. Air Force, AFWAL, Wright-Patterson, OH.
Advanced swirl concepts for ramjets
