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High Technology Corporation

Company Information
Address
28 Research Drive
Hampton, VA 23666
United States



Information

UEI: N/A

# of Employees: 6


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: Yes

Woman Owned: No



Award Charts




Award Listing

  1. Active Suppression of Resonance Interactions between Shear-Layers and Cavities

    Amount: $68,801.00

    N/A

    SBIRPhase I1994National Aeronautics and Space Administration
  2. Supersonic Jet-Noise Prediction and Control

    Amount: $68,458.00

    N/A

    SBIRPhase I1994National Aeronautics and Space Administration
  3. Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

    Amount: $485,880.00

    N/A

    SBIRPhase II1994National Aeronautics and Space Administration
  4. Transition Prediction and Laminar Flow Control in Compressible 3D Boundary Layers Using PSE

    Amount: $49,927.00

    N/A

    SBIRPhase I1993National Aeronautics and Space Administration
  5. NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

    Amount: $179,309.00

    IT IS PROPOSED HERE TO STUDY NONLINEAR DEVELOPMENT OF GORTLER AND CROSSFLOW VORTICES AND INVESTIGATE VARIOUS WAVE-INTERACTION MECHANISMS OPERATIVE IN TWO AND THREE-DIMENSIONAL BOUNDARY LAYERS. THE PRO ...

    SBIRPhase II1990Department of Defense Air Force
  6. ADVANCED COMPUTATIONAL TECHNIQUES IN STUDIES OF HYPERSONIC BOUNDARY-LAYER TRANSITION

    Amount: $49,994.00

    THE OBJECTIVE OF THE PROPOSED WORK IS TO USE ADVANCED THEORETICAL AND COMPUTATIONAL TECHNIQUES FOR STUDIES OF HYPERSONIC BOUNDARY LAYER STABILITY AND TRANSITION TO TURBULENCE. THESE STUDIES WILL ENHAN ...

    SBIRPhase I1990Department of Defense Air Force
  7. NUMERICAL AND ANALYTIAL STUDIES OF LAMINAR TO TURBULENCE TRANSITION

    Amount: $49,920.00

    N/A

    SBIRPhase I1989Department of Defense Air Force
  8. STABILITY AND TRANSITION IN CHEMICALLY REACTING NONEQUILIBRIUM FLOWS

    Amount: $50,608.00

    IT IS PROPOSED HERE TO DEVELOP A METHOD FOR PREDICTION OF TRANSITION ON NASP (NATIONAL AERO-SPACE PLANE) CONFIGURATION AND FOR THE CONTROL/ENHANCEMENT OF SUPERSONIC COMBUSTION IN THE SCRAMJET. THE MET ...

    SBIRPhase I1988Department of Defense Defense Advanced Research Projects Agency
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