The Online Books Page

Books by Douglas R. Lord:

Books in the extended shelves:

• Lord, Douglas R.: Aerodynamic characteristics of a spoiler-slot-deflector control on a 45° sweptback wing at Mach numbers of 1.61 and 2.01 (National Advisory Committee for Aeronautics, 1957), also by Robert Moring, United States. National Adviosry Committee for Aeronautics, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lord, Douglas R.: Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds (National Advisory Committee for Aeronautics, 1949), also by Bernard N. Daley, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lord, Douglas R.: Load distributions associated with controls at supersonic speeds (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lord, Douglas R.: Loads associated with spoilers at supersonic speeds (National Advisory Committee for Aeronautics, 1955), also by K. R. Czarnecki, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lord, Douglas R.: Recent information on flap and tip controls (National Advisory Committee for Aeronautics, 1953), also by K. R. Czarnecki, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lord, Douglas R.: Spacelab, an international success story (Scientific and Technical Information Division, National Aeronautics and Space Administration :, 1987), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Lord, Douglas R.: Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01 (National Aeronautics and Space Administration, 1959), also by K. R. Czarnecki and Langley Research Center (page images at HathiTrust)

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