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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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High Speed Flight Control Techniques
Amount: $498,364.00The development of innovative control techniques required for next generation maneuvering high speed vehicles is proposed.The Armys requirement for future hypersonic vehicles with enhanced maneuverabi ...
SBIRPhase II2017Department of Defense Army -
Simulation Tool for Turbomachinery Operating with Trans-Critical Real Fluids
Amount: $149,998.78The SCO2 Brayton cycle is gaining interest across a variety of power generation applications due to its potential for providing higher efficiencies. The range of industrial applications include: indus ...
SBIRPhase I2016Department of Energy -
Reduced-Order Inflow Model for Propeller-Airframe Flow Interaction Noise Assessment
Amount: $99,998.17In Phase I, our research team will focus on the fundamental interaction of the wake from a horizontal flat plate with a pusher-prop, using experimental and numerical techniques.The experimental campai ...
SBIRPhase I2016Department of Defense Army -
Innovative Hypervelocity Control Techniques for future Army Aerospace Vehicle
Amount: $149,999.05The development of innovative control concepts required for next generation maneuvering hypervelocity vehicles is proposed.The Armys requirement for future hypersonic vehicles with enhanced maneuverab ...
SBIRPhase I2016Department of Defense Army -
Ceramic Matrix Composite Materials for Transpiration Cooling
Amount: $993,875.00The proposed effort will formulate and demonstrate the methodology for fabricating Porous Ceramic Matrix Composite (PCMC) transpiration plates with controlled levels of porosity, suitable for high-spe ...
SBIRPhase II2016Department of Defense Army -
Afterburning Missile Base Flow Modeling and Analyses
Amount: $999,999.75A validated, advanced, detailed physics-based CFD capability to accurately model the separated flow physics immediately downstream in the base region of a propulsive supersonic/hypersonic missile with ...
SBIRPhase II2016Department of Defense Army -
Unsteady Airfoil Design Optimization with Application to Dynamic Stall
Amount: $999,998.50Dynamic stall in rotorcraft blades still remains a challenging problem for the US Army since it limits the operability, maneuverability and flight speed of the rotorcraft. There are numerous documente ...
SBIRPhase II2016Department of Defense Army -
Navy Air Cushions Vehicles (ACVs) Lift Fan Impeller Optimization
Amount: $80,000.00The lift fan system is an integral part of the hovercraft class of vehicles such as Ship-to-Shore Connector (SSC) and is used to pressurize the skirt and discharge air to the thrusters for steering. A ...
SBIRPhase I2016Department of Defense Navy -
Response Surface Modeling of Aerodynamic Interference Effects for Refueling Scenarios
Amount: $149,999.00Aerial refueling is a mission-critical component of Navy operations. The refueling portion of a mission is made difficult by the inherent interference between the tanker and receiver aircraft. The rec ...
SBIRPhase I2016Department of Defense Navy -
Reduced-Order Kinetic Models for Real Fuels Applicable to High-Pressure Turbulent Flows
Amount: $149,996.00Gas turbine combustion plays an important role in a range of Army systems critical to fulfilling the Armys strategic mission. Since high-performance gas turbine propulsion systems operate under highly ...
STTRPhase I2016Department of Defense Army
