Search results for: Blair, A. B.

Showing 1 - 7 results of 7 Refine Results
  1. 1

    Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1980
    Physical Description: 197 pages : chiefly illustrations ; 27 cm.
    Government Document Microfilm Book
  2. 2

    Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985
    Physical Description: 1 volume.
    Government Document Microfilm Book
  3. 3

    Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Physical Description: 83 pages : illustrations ; 28 cm.
    Government Document Book
  4. 4

    Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Physical Description: 101 pages : illustrations ; 27 cm.
    Government Document Book
  5. 5

    Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Physical Description: 76 pages : illustrations ; 27 cm.
    Government Document Book
  6. 6

    An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979
    Physical Description: 188 pages : illustrations ; 27 cm.
    Government Document Book
  7. 7

    Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate

    Authors: Blair, A. B.
    Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; For sale by the National Technical Information Service, 1986
    Physical Description: 1 volume.
    Government Document Microfilm Book