Showing 1 - 5 results of 5 for search 'Sawyer, Wallace C.', query time: 0.04s Refine Results
  1. 1
    Stability and control characteristics of a monoplanar elliptic missile model at Mach numbers from 1.60 to 2.86

    Stability and control characteristics of a monoplanar elliptic missile model at Mach numbers from 1.60 to 2.86 by Sawyer, Wallace C.

    Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


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  2. 2
    Investigation of flow characteristics over missile bodies at supersonic speeds

    Investigation of flow characteristics over missile bodies at supersonic speeds by Barger, Raymond L.

    Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service], 1979
    Other Authors: “…Sawyer, Wallace C.…”
    Format: Government Document Book


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  3. 3
    Longitudinal aerodynamic characteristics at Mach numbers from 1.60 to 2.86 for a spanmissile with three wing planforms

    Longitudinal aerodynamic characteristics at Mach numbers from 1.60 to 2.86 for a spanmissile with three wing planforms by Spearman, M. Leroy

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Information Service, 1977
    Other Authors: “…Sawyer, Wallace C.…”
    Format: Government Document Book


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  4. 4
    Investigation of flow characteristics over missle bodies at supersonic speeds

    Investigation of flow characteristics over missle bodies at supersonic speeds by Barger, Raymond L.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979
    Other Authors: “…Sawyer, Wallace C.…”
    Format: Government Document Book


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  5. 5
    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements

    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements by Lamb, Milton

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Other Authors: “…Sawyer, Wallace C.…”
    Format: Government Document Book


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