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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. 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
  2. Coupled Pyrolysis, Radiant Heat Transfer, and Fluid Dynamics Modeling

    Amount: $999,998.40

    The primary goal of this SBIR Phase II proposal is to provide the Army with a dramatically enhanced ability to accurately predict IR emissions and radiant heat transfer for missile plume and missile b ...

    SBIRPhase II2017Department of Defense Army
  3. Variable Pressure/Flow Control Firefighting Nozzle

    Amount: $149,997.00

    Combustion Research and Flow Technology (CRAFT Tech) and its partner, Vulcan Research & Controls (VRC) propose the development of a hybrid firefighting hand nozzle providing both Ultra-High Pressure ( ...

    SBIRPhase I2017Department of Defense Air Force
  4. Ignition Modeling for Present and Future Combustors and Augmentors

    Amount: $224,996.00

    The primary objective of this effort is to develop a tractable computational tool to assess the probability of ignition within aircraft combustors and augmentors during routine igniter and/or system d ...

    STTRPhase I2017Department of Defense Navy
  5. Reduced-Order Airwake Modeling for Aircraft/Ship Integration Modeling and Simulation

    Amount: $224,999.00

    The objective of this STTR research program is to develop a reduced order modeling (ROM) approach for efficiently and accurately representing computed CFD ship airwake data. This approach will enable ...

    STTRPhase I2017Department of Defense Navy
  6. Uncertainty-Analysis-Driven Reduced-Order Kinetic Models Targeting Combustion Dynamics

    Amount: $149,999.00

    The design and development of a number of advanced Air Force propulsion systems is substantially limited by the current inability of computational design support tools to adequately and cost-effective ...

    STTRPhase I2017Department of Defense Air Force
  7. Phase Transitions, Nucleation and Mixing Modeling through Trans-Critical Conditions

    Amount: $749,999.00

    The goal of this Phase II effort is to achieve significant improvements in our understanding and modeling of trans-critical combustors operating at high pressure in regimes of interest to the Air Forc ...

    STTRPhase II2017Department of Defense Air Force
  8. High Speed Flight Control Techniques

    Amount: $498,364.00

    The 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
  9. Simulation Tool for Turbomachinery Operating with Trans-Critical Real Fluids

    Amount: $149,998.78

    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 I2016Department of Energy
  10. Reduced-Order Inflow Model for Propeller-Airframe Flow Interaction Noise Assessment

    Amount: $99,998.17

    In 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
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