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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. Novel Concepts for a CFD-Enhanced ASTROS Capability

    Amount: $76,223.00

    The proposed research will determne the feasibility of extending the steady and unsteady aerodynamic modeling capabilities of ASTROs using modern nonlinear Computational Fluid Dynamics. The object of ...

    SBIRPhase I1995Department of Defense Air Force

  2. Electronic Knowledge Exchange System For Cfd Validation Concepts

    Amount: $68,978.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration

  3. Development of an Indicial Prediction System for Unsteady Aerodynamic Modeling in Simulation and Design of Maneuvering Fighter Aircraft Co

    Amount: $68,539.00

    N/A

    SBIRPhase I1995Department of Defense Air Force

  4. Similarity Principles To Enable Heavy Gas Testing Of High-Lift Systems At Flight Reynolds Numbers

    Amount: $68,930.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration

  5. Turbulence Model With Enhanced Physics And Neural Network Closure Modeling

    Amount: $69,916.00

    N/A

    SBIRPhase I1995National Aeronautics and Space Administration

  6. COMPUTATIONAL METHODOLOGY FOR MANEUVERING AIRCRAFT

    Amount: $358,204.00

    THE PHASE I INVESTIGATION WILL DEMONSTRATE THE FEASIBILITY OF AN ANALYTICAL APPROACH TO PREDICT THE HIGH ANGLE-OF-ATTACK AERODYNAMIC CHARACTERISTICS OF AGILE FIGHTER AIRCRAFT AND TACTICAL MISSILES IN ...

    SBIRPhase II1994Department of Defense Defense Advanced Research Projects Agency

  7. Optimal Aerodynamic Design of Missile Fins with Geometric Constraints

    Amount: $382,704.00

    Within DoD there is a current need for the design or redesign of aircraft-borne weapon airframes to meet conformal/internal carriage requirements. A major constraint imposed by confromal/internal carr ...

    SBIRPhase II1994Department of Defense Air Force

  8. Similified, Vorticity-Enhanced, Potential-Flow Method for Early Design and Analysis of Maneuvering Aircraft

    Amount: $70,000.00

    Maneuvering aircraft at high angles of attack experience severeunsteady loading. This loading, when unanticipated at the designstage, can cause fatigue problems and, possibly, structuralfailure. Such ...

    SBIRPhase I1994National Aeronautics and Space Administration

  9. Aircraft Drag Reduction Using a MEMS-Based Flow Control Device

    Amount: $60,000.00

    Drag reduction via active control of wing boundary layers will result in substantial performance and range improvements for both military and commercial aircraft. The increased efficiency will reduce ...

    SBIRPhase I1994Department of Defense Air Force

  10. DRAG REDUCTION IN PIPES USING NONLINEAR FLOW STATES

    Amount: $65,000.00

    DRAG DUE TO TURBULENT SKIN FRICTION SUBSTANTIALLY PENALIZES THE PERFORMANCE AND ECONOMICS OF OIL AND GAS PIPELINES. USING TWO NEW CONTROL IDEAS ORIGINATING FROM RESEARCH IN NONLINEAR DYNAMICAL SYSTEM ...

    SBIRPhase I1994National Science Foundation
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