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NIELSEN ENGINEERING & RESEARCH, INC.

Company Information
Address
900 LAFAYETTE ST
SANTA CLARA, CA 95050-4934
United States
Information

UEI: N/A

# of Employees: 4
Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No

Award Charts




Award Listing

  • Record 1 TO 121

  1. METHODS OF COMPUTATIONAL AEROACCOUSTICS

    Amount: $50,000.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration

  2. SURFACE ROUGHNESS FEATURES FORMULATION FOR AIRCRAFT ICING

    Amount: $49,848.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration

  3. A MATHEMATICALLY BASED REYNOLDS-STRESS MODEL OF TURBULENCE

    Amount: $50,000.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration

  4. COMPUTATIONAL METHODOLOGY FOR MANEUVERING AIRCRAFT

    Amount: $67,180.00

    N/A

    SBIRPhase I1992Department of Defense Defense Advanced Research Projects Agency

  5. A PREDICTION METHOD FOR HIGH ANGLE OF ATTACH AERODYNAMICS

    Amount: $49,870.00

    N/A

    SBIRPhase I1992National Aeronautics and Space Administration

  6. UNSTRUCTURED TRIANGULAR MESH/NAVIER-STOKES METHOD FOR AERODYNAMICS OF AIRCRAFT WITH ICE ACCRETION

    Amount: $403,790.00

    ICE ACCRETION ON COMPONENTS OF BOTH FIXED WING AIRCRAFT AND ROTORCRAFT CAN CAUSE AERODYNAMIC PENALTIES SUCH AS INCREASEDDRAG, DECREASED LIFT, REDUCED STALL ANGLE, INCREASED STALL SPEED AND INCREASED E ...

    SBIRPhase II1991National Aeronautics and Space Administration

  7. NONLINEAR CONTROL OF SHEAR FLOWS

    Amount: $50,000.00

    N/A

    SBIRPhase I1991National Aeronautics and Space Administration

  8. A COMPUTATIONAL MODEL FOR THRUST REVERSING AND VECTORED JETS

    Amount: $182,533.00

    BECAUSE OF RECENTLY DEFINED TACTICAL THREATS IT IS DESIRABLE TO IMPROVE THE MANEUVERABILITY AND TAKE-OFF/LANDING ASPECTS OF AIRCRAFT PERFORMANCE. IT HAS BEEN DETERMINED THAT SUCH IMPROVEMENTS CAN BE A ...

    SBIRPhase II1990Department of Defense Air Force

  9. A MODEL FOR SHOCK TURBULENCE INTERACTION

    Amount: $50,000.00

    ONE OF THE MOST IMPORTANT ISSUES IN DEVELOPING COMPUTATIONALFLUID DYNAMICS FOR HYPERSONIC FLOW IS TURBULENCE MODELING. ONE OF THE UNIQUE ASPECTS OF HYPERSONIC FLOW IS THE EFFECT OF THE SHOCK WAVES ON ...

    SBIRPhase I1990National Aeronautics and Space Administration

  10. ADVANCED METHODS FOR ATMOSPHERIC MODELING

    Amount: $50,000.00

    ATMOSPHERIC SCIENCE INVOLVES STUDIES OF VERY COMPLEX PHYSICAL PROCESSES. OFTEN, SIMPLIFIED VERSIONS OF THESE PROCESSES ARE SIMULATED IN A LABORATORY OR ON A COMPUTER. COMPUTATIONAL FLUID DYNAMICS (CFD ...

    SBIRPhase I1990Department of Defense Air Force
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