The Online Books Page

Books by Alan B. Kehlet:

Books in the extended shelves:

• Kehlet, Alan B.: Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail (Washington, D.C. : National Advisory Committee for Aeronautics, 1954., 1954), also by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Kehlet, Alan B.: Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Kehlet, Alan B.: Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail. (National Advisory Committee for Aeronautics, 1958), also by United States. National Adviosry Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Kehlet, Alan B.: Longitudinal stability and trim of two rocket-propelled airplane models having 45° sweptback wings and tails with the horizontal tail mounted in two positions (National Advisory Committee for Aeronautics, 1953), also by James H. Parks, United States. National Adviosry Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)

Find more by Alan B. Kehlet at your library, or elsewhere.