Showing 1 - 10 results of 19 for search 'Shrout, Barrett L', query time: 0.23s Refine Results
  1. 1
    Aerodynamic characteristics at Mach numbers from 0.6 to 2.16 of supersonic cruise fighter configuration with a design Mach mumber of 1.8 /
    by Shrout, Barrett L
    Published 1977

    Government Document Book
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  2. 2
    Effect of a simulated engine jet blowing above an arrow wing at mach 2.0 /
    by Shrout, Barrett L
    Published 1978

    Government Document Book
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  3. 3
    Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 /
    by Shrout, Barrett L
    Published 1982

    Government Document Book
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  4. 4
    Aerodynamic characteristics of a series of bodies with variations in nose camber /
    by Shrout, Barrett L
    Published 1983

    Government Document Book
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  5. 5
    A wind-tunnel investigation of sonic-boom pressure distributions of bodies of revolution at Mach 2.96, 3.83, and 4.63 /
    by Shrout, Barrett L
    Published 1971

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
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  6. 6
    Aerodynamic characteristics at Mach numbers from 0.6 to 2.16 of supersonic cruise fighter configuration with a design Mach mumber of 1.8 /
    by Shrout, Barrett L
    Published 1977

    Government Document Book
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  7. 7
    Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30 /
    by Shrout, Barrett L
    Published 1979

    Government Document Book
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  8. 8
    Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30 /
    by Shrout, Barrett L
    Published 1979

    Government Document Book
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  9. 9
    A wind-tunnel investigation of sonic-boom pressure distributions of bodies of revolution at Mach 2.96, 3.83, and 4.63,
    by Shrout, Barrett L
    Published 1971

    Book
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  10. 10
    Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63 /
    by Shrout, Barrett L
    Published 1982

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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    Saved in:
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