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COMBUSTION RESEARCH & FLOW TECHNOLOGY INC
UEI: XGYZK5MHNJZ8
# of Employees: 24
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Transient, Rocket Exhaust Plume Modeling for Static Test Analyses
Amount: $729,998.00Our proposal addresses the high fidelity modeling of transient rocket exhaust plumes in a static test environment. Static testing provides a practical means of obtaining plume signature data to suppor ...
SBIRPhase II2011Department of Defense Army -
Development of a Computational Method for Prediction of After-Burning Effect
Amount: $69,928.00The problem of interest is the development of a physics based model for conducting high-fidelity simulation of afterburning munitions, which are unique in that that they contain solid and/or liquid fu ...
STTRPhase I2010Department of Defense Navy -
High-Fidelity Simulation of Dynamic Weakly Ionized Plasma Phenomena
Amount: $99,992.00In the Phase I program, we will design an experiment/test article, and test/validate instrumentation and diagnostics, to be used to obtain plasma properties about a hypersonic vehicle having character ...
STTRPhase I2010Department of Defense Air Force -
Plume EO-RCS Data Fusion
Amount: $99,946.00Characteristics of missile plume UV/Visible emissions & RCS have a great potential to enhance defensive capabilities in several areas related to Ballistic Missile Defense Systems (BMDS). Supporting MD ...
SBIRPhase I2010Department of Defense Missile Defense Agency -
Effects of Hardbody-Plume Interactions on Radar Returns
Amount: $99,995.00The innovation in this proposal relates to the use of a generalized framework for prediction of RCS that utilizes a common procedure for computing the signature from a hardbody and its associated plum ...
SBIRPhase I2010Department of Defense Missile Defense Agency -
Large Eddy Simulations of Hot Supersonic Jets for Aeroacoustics
Amount: $499,924.00The noise from the turbulent, hot, supersonic jets at take-offs and landings as well as high-Mach cruise at altitude dominates noise emanating from other powerplant components and has significant safe ...
STTRPhase II2010Department of Defense Navy -
Uncertainty Quantification for Production Navier-Stokes Solvers
Amount: $99,991.00Solution errors are inherent in any Computational Fluid Dynamics (CFD) simulation. Systematic identification, reduction, and control of these various error sources is crucial if the results of CFD si ...
SBIRPhase I2010National Aeronautics and Space Administration -
Efficient Implementation of Models for Improved Prediction of Gas Turbine Combustor and Augmentor Robustness
Amount: $99,995.00The technical objective of this program is to develop a fast running, subgrid scale turbulence-chemistry interaction model for large-eddy simulation (LES) of aircraft combustors and augmentors that ca ...
SBIRPhase I2010Department of Defense Air Force -
High Speed Store Separation Data Acquisition Techniques
Amount: $99,976.00The development of diagnostic techniques to simultaneously measure store trajectories and instantaneous flow state during store dispense at high speeds (Mach 2.0-5.0) from weapons bays is proposed. In ...
SBIRPhase I2010Department of Defense Air Force -
Integrated Component and System Analyses of Instabilities in Test Stands
Amount: $599,998.00Instabilities associated with the operation of liquid rocket propulsion systems and test facilities usually manifest themselves as structural vibrations and may cause structural damage. While the sour ...
STTRPhase II2010National Aeronautics and Space Administration
