Showing 1 - 14 results of 14 for search 'Miller, David S. (Of Langley Research Center)', query time: 0.05s Refine Results
  1. 1
    A study of the application of heat or force fields to the sonic-boom-minimization problem /

    A study of the application of heat or force fields to the sonic-boom-minimization problem / by Miller, David S. (Of Langley Research Center)

    Published 1969
    Government Document Book
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  2. 2
    Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /

    Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Sorrells, Russell B., Miller, David S. (Of Langley Research Center)

    Published 1972
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  3. 3
    Lee-side flow over delta wings at supersonic speeds /

    Lee-side flow over delta wings at supersonic speeds / by Miller, David S. (Of Langley Research Center), Wood, Richard M.

    Published 1985
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  4. 4
    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept

    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.

    Published 1983
    Government Document Microfilm Book
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  5. 5
    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept / by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.

    Published 1983
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  6. 6
    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /

    Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept / by Wood, Richard M., Miller, David S. (Of Langley Research Center), Brentner, Kenneth S.

    Published 1983
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  7. 7
    Numerical methods for the design and analysis of wings at supersonic speeds

    Numerical methods for the design and analysis of wings at supersonic speeds by Carlson, Harry W.

    Published 1974
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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  8. 8
    Wing planform effects at supersonic speeds for an advanced fighter configuration /

    Wing planform effects at supersonic speeds for an advanced fighter configuration / by Wood, Richard M.

    Published 1984
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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  9. 9
    Experimental investigation of leading-edge thrust at supersonic speeds /

    Experimental investigation of leading-edge thrust at supersonic speeds / by Wood, Richard M.

    Published 1983
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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  10. 10
    Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /

    Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /

    Published 1981
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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  11. 11
    Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations /

    Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations / by Wood, Richard M.

    Published 1984
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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  12. 12
    Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /

    Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Sorrells, Russell B.

    Published 1972
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
    Government Document Book
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  13. 13
    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards /

    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / by Robins, A. Warner

    Published 1979
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  14. 14
    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /

    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 / by Pittman, Jimmy L.

    Published 1984
    Other Authors: “…Miller, David S. (Of Langley Research Center)…”
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