Search results for: Covell, Peter F.

Showing 1 - 10 results of 10 Refine Results
  1. 1

    Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50

    Authors: Covell, Peter F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982
    Physical Description: 32 pages : illustrations ; 28 cm.
    Government Document Book
  2. 2

    Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

    Authors: Covell, Peter F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1987
    Physical Description: 1 volume.
    Government Document Microfilm Book
  3. 3

    Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5

    Authors: Covell, Peter F.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
    Physical Description: 1 volume.
    Government Document Microfilm Book
  4. 4

    Interference effects of aft reaction-control yaw jets on the aerodynamic characteristics of a space shuttle orbiter model at supersonic speeds

    Authors: Covell, Peter F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Physical Description: 44 pages : illustrations ; 28 cm.
    Government Document Book
  5. 5

    Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16

    Authors: Wood, Richard M., Covell, Peter F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Physical Description: 1 online resource (119 pages) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  6. 6

    Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16

    Authors: Wood, Richard M., Covell, Peter F.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Physical Description: 1 online resource (119 pages, 1 unnumbered page) : illustrations.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Electronic eBook
  7. 7

    Effects of winglets on a first-generation jet transport wing : VII, sideslip effects on winglet loads and selected wing loads at subsonic speeds for a full-span model

    Authors: Meyer, Robert R.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Other Authors: “…Covell, Peter F.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  8. 8

    Aerodynamic characteristics of a series of bodies with variations in nose camber

    Authors: Shrout, Barrett L.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Other Authors: “…Covell, Peter F.…”
    Physical Description: 52 pages : illustrations ; 28 cm.
    Government Document Book
  9. 9

    Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16

    Authors: Wood, Richard M.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1985
    Other Authors: “…Covell, Peter F.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book
  10. 10

    Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

    Authors: Walker, Ira J.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993
    Other Authors: “…Covell, Peter F.…”
    Physical Description: 1 volume.
    Government Document Microfilm Book