The Online Books Page

Online Books by

A. B. Blair

• Blair, A. B.: Wind-Tunnel Investigation at Supersonic Speeds of a Canard-Controlled Missile with Fixed and Free-Rolling Tail Fins (NASA Technical Paper 1316; 1978) (page images at HathiTrust)

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Additional books from the extended shelves:

• Blair, A. B.: Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 ̊clipped-delta-wing orbiter configuration at supersonic mach numbers (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration and Langley Research Center (page images at HathiTrust)
• Blair, A. B.: Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Blair, A. B.: Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Gloria Hernandez, Jerry M. Allen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Blair, A. B.: An experimental wind-tunnel investigation of a ram-air-spoiler roll-control device on a forward-control missile at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Blair, A. B.: Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86 (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Blair, A. B.: Wind-tunnel investigation at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control (NASA Langley Research Center, 1978) (page images at HathiTrust; US access only)

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