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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. Highly Compact Supersonic Cruise Missile (SSCM) Engine Inlet

    Amount: $149,989.00

    As air vehicle speeds increase, air breathing engine and inlet technology follow through concurrent supersonic performance requirements. The recent ability to build smaller supersonic engines has esta ...

    SBIRPhase I2012Department of Defense Navy
  2. Aeroacoustics of High-Speed Jet Impingement

    Amount: $749,928.00

    The noise from the turbulent, hot, supersonic jets at take-offs and landings dominates noise emanating from other powerplant components and has significant safety implications for launch personnel, as ...

    SBIRPhase II2012Department of Defense Navy
  3. Rotor-Airwake Aerodynamic Coupling in Real-Time Simulation

    Amount: $749,904.00

    An innovative approach for incorporating the coupled interaction between a ship airwake and rotor downwash in real-time dynamic interface simulations is proposed. The approach employs a database of hi ...

    SBIRPhase II2012Department of Defense Navy
  4. Coupled Pyrolysis, Radiant Heat Transfer, and Fluid Dynamics Modeling

    Amount: $149,981.00

    The proposed Phase I effort involves the formulation of an advanced model for accurately simulating the post burn out effects in solid rocket motors. This all encompassing model will account for known ...

    SBIRPhase I2012Department of Defense Army
  5. Unsteady Airfoil Design Optimization with Application to Dynamic Stall

    Amount: $999,929.00

    One of the most persistent problems affecting the aerodynamic performance of rotorcrafts is retreating blade stall that results in large pitching moments and hazardous control situations. In this pro ...

    SBIRPhase II2012Department of Defense Army
  6. Coupled Pyrolysis, Radiant Heat Transfer, and Fluid Dynamics Modeling

    Amount: $990,315.00

    The Phase II effort will unify advanced models for simulating post burn out effects in solid rocket motors (SRM"s), coupling fluid dynamic, radiative, and conductive heat transfer processes using inno ...

    SBIRPhase II2012Department of Defense Army
  7. Uncertainty Quantification for Production Navier-Stokes Solvers

    Amount: $599,983.00

    The uncertainty quantification methods developed under this program are designed for use with current state-of-the-art flow solvers developed by and in use at NASA. The Phase I program demonstrated t ...

    SBIRPhase II2011National Aeronautics and Space Administration
  8. Novel Design of Orifice Type Control Element for Mitigating Instabilities

    Amount: $99,971.00

    An orifice element is commonly used in liquid rocket engine test facilities either as a flow metering device, or to provide a large reduction in pressure over a very small distance in the piping syste ...

    STTRPhase I2011National Aeronautics and Space Administration
  9. A Generalized Software Toolkit for Portable GPU-Enabled Chemistry Acceleration in CFD Applications

    Amount: $99,995.00

    Current combustor design simulations aimed at reducing greenhouse gas emissions and improving fuel-lean combustion have entailed using large amounts of dedicated CPU resources for extended time period ...

    SBIRPhase I2011National Aeronautics and Space Administration
  10. Design Support and Analysis Tool for Pyrotechnically Actuated Valves

    Amount: $99,984.00

    Pyrotechnically actuated valves are triggered on or off by firing an explosive charge that rapidly releases large amounts of high-pressure, gas. Pyrovalves are generally used for critical safety func ...

    SBIRPhase I2011National Aeronautics and Space Administration
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