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COMBUSTION RESEARCH AND FLOW TECHNOLOGY INC

Company Information
Address
6210 KELLERS CHURCH RD
PIPERSVILLE, PA 18947-1020
United States


http://www.craft-tech.com

Information

DUNS: 929950012

# of Employees: 32


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Low-Order Models for the Evolution of Scalar and Vector Quantities in Supersonic Particle Laden Plumes

    Amount: $149,997.44

    Missile base flow prediction is an area that has eluded a satisfactory solution since the 1950's owing to the complex aero-thermo-chemical physics of this region involving flow separation, two-phase g ...

    SBIRPhase I2018Department of Defense Army
  2. Observable Signatures of Missile Threats to Army Interests in the Field

    Amount: $149,997.45

    The primary objective of this effort is to develop an advanced turbulent combustion model to accurately capture local flame extinction effects that result in afterburning missile plume flame lifting a ...

    SBIRPhase I2018Department of Defense Army
  3. Time-Resolved, Reynolds-Average Navier Stokes (RANS) / Large Eddy Simulation (LES) Flow-Modeling Tools Suitable for Gas Turbine Engine Sand and Dust M

    Amount: $749,999.00

    A Reactive Solids Tool concept will be developed which can be interfaced with a modern high-fidelity Computational Fluid Dynamics code to predict sand and ash behavior in high temperature combustor en ...

    SBIRPhase II2018Department of Defense Navy
  4. Subtopic Letter (d) Combustion Modeling for Direct Fired Supercritical CO2 Power Cycles

    Amount: $154,994.00

    The 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 I2017Department of Energy
  5. Simulation Tool for Turbomachinery Operating with Trans-Critical Real Fluids

    Amount: $999,999.00

    The SCO2 Brayton cycle is gaining interest across a variety of power generation applications due to its potential for providing higher efficiencies. These applications require compressors that operate ...

    SBIRPhase II2017Department of Energy
  6. A Software Toolkit to Accelerate Emission Predictions for Turboelectric/Hybrid Electric Aircraft Propulsion

    Amount: $125,000.00

    Electric propulsion represents an attractive path for reducing overall emissions. For larger commercial aircrafts operating in the mega-watt range, power turboelectric and hybrid electric aircraft pro ...

    SBIRPhase I2017National Aeronautics and Space Administration
  7. Modeling Turbulence Effects in Cryogenic Propellant Tank Thermal Management

    Amount: $124,999.00

    Control and management of cryogenic propellant tank pressures in low gravity is an important technical challenge to overcome for future long duration space missions. Advanced techniques such as thermo ...

    SBIRPhase I2017National Aeronautics and Space Administration
  8. Modeling of Complex Endo-atmospheric Wakes

    Amount: $100,000.00

    Threat signature phenomenology plays an important role in the development of missile defense technologies, both at tactical and strategic levels. However, threats from non-traditional, non-symmetric ...

    SBIRPhase I2017Department of Defense Missile Defense Agency
  9. Time-Resolved, Reynolds-Average Navier Stokes (RANS) / Large Eddy Simulation (LES) Flow-Modeling Tools Suitable for Gas Turbine Engine Sand and Dust M

    Amount: $224,998.00

    A Reactive Solids Tool concept will be developed which can be interfaced with a modern high-fidelity Computational Fluid Dynamics code to predict sand and ash behavior in high temperature combustor en ...

    SBIRPhase I2017Department of Defense Navy
  10. Unsteady Flow Analysis on Inlet and Exhaust System Distortion and Structural Analysis for Modern Propulsion Systems

    Amount: $749,996.00

    Modern aircraft and rotorcraft feature tightly integrated propulsion systems, with engine inlet and exhaust geometries that are complex and designed to meet multiple objectives. Unsteady flows through ...

    SBIRPhase II2017Department of Defense Navy
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