More about Harold S. Johnson:
| | Books by Harold S. Johnson: Books in the extended shelves: Johnson, Harold S.: Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6° and NACA 65A006 airfoil section (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Johnson, Harold S.: Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons (National Advisory Committee for Aeronautics, 1951), also by John R. Hagerman and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Johnson, Harold S.: Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45° sweptback-wing--body combination (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by Langley Aeronautical Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Johnson, Harold S.: Wind-tunnel investigation of the effects of various dorsal-fin and vertical-tail configurations on the directional stability of a streamlined body at transonic speeds, transonic-bump method (Washington, D.C. : National Advisory Committee for Aeronautics, 1953., 1953), also by William C. Hayes, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
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