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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

  1. A NOVEL POTENTIAL/VISCOUS FLOW COUPLING TECHNIQUE FOR COMPUTING HELICOPTER FLOW FIELDS

    SBC: Targazyme, Inc.            Topic: N/A

    BECAUSE OF THE COMPLEXITY OF THE HELICOPTER FLOW FIELD, A ZONAL METHOD OF ANALYSIS OF COMPUTATIONAL AERODYNAMICS IS REQUIRED. IN THIS RESEARCH, A NEW PROCEDURE FOR COUPLING POTENTIAL AND VISCOUS FLOW CALCULATION SCHEMES IS PROPOSED. AN OVER-LAPPING, VELOCITY-COUPLING TECHNIQUE IS TO BE DEVELOPED WITH THE UNIQUE FEATURE THAT THE POTENTIAL FLOW SURFACE SINGULARITY STRENGTHS ARE OBTAINED DIRECTLY FRO ...

    SBIR Phase II 1990 National Aeronautics and Space Administration
  2. Error Reduction For Pressure-Sensitive Paint Applications

    SBC: Applied Sciences Inc.            Topic: N/A

    N/A

    SBIR Phase II 1996 National Aeronautics and Space Administration
  3. Aircraft Drag Reduction Using Distributed Suction And Adaptive Control Techniques

    SBC: Innovative Aerodynamic            Topic: N/A

    N/A

    SBIR Phase II 1996 National Aeronautics and Space Administration
  4. A NONINTRUSIVE REAL TIME ROCKET PLUME DIAGNOSTIC USING NEAR-INFRARED DIODE LASER SENSORS

    SBC: Southwest Sciences, Inc.            Topic: N/A

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
  5. AN ACTIVE CONTROL STICK WITH PILOT FORCE CUEING FOR AGILE HELICOPTERS

    SBC: SDI Engineering Inc            Topic: N/A

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
  6. A Combined Micro-Mechanics, Fracture Mechanics, And Statistical Approach For Life Prediction Of Ceramic Matrix And Metal Matrix Composites

    SBC: Tao Of Systems Integration Inc            Topic: N/A

    N/A

    SBIR Phase II 1996 National Aeronautics and Space Administration
  7. INTERACTIVE FLOW MEARSUREMENT (IFM) SYSTEM FOR HIGH REYNOLDS NUMBER WIND TUNNEL TESTING

    SBC: Tao Of Systems Integration Inc            Topic: N/A

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
  8. AUTOMATED HOT-WIRE ANEMOMETER INSTRUMENTATION SYSTEM FOR IN-FLIGHT VELOCITY FLOW FIELD MEASUREMENTS

    SBC: Tao Of Systems Integration Inc            Topic: N/A

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
  9. PREDICTABLE REAL-TIME MULTIPROCESSING IN AIRBORNE SYSTEMS

    SBC: Unisoft Consulting Inc            Topic: N/A

    N/A

    SBIR Phase I 1996 National Aeronautics and Space Administration
  10. A 3D MOVING MAP FOR GA COCKPITS

    SBC: Vision Micro Design Inc            Topic: N/A

    N/A

    SBIR Phase II 1997 National Aeronautics and Space Administration
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