The Online Books Page

Pitch (inclination)

See also what's at your library, or elsewhere.

• Moving-cockpit simulator investigation of the minimum tolerable longitudinal maneuvering stability (National Aeronautics and Space Administration, 1959), by B. Porter Brown, Harold I. Johnson, and Langley Research Center (page images at HathiTrust)
• Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 (National Aeronautics and Space Administration, 1959), by Clarence L. Gillis, A. James Vitale, and Langley Research Center (page images at HathiTrust)
• A simulator study of the effectiveness of a pilot's indicator which combined angle of attack and rate of change of total pressure as applied to the take-off rotation and climbout of a supersonic transport (National Aeronautics and Space Administration, 1961), by Albert W. Hall, Jack E. Harris, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Wind-tunnel and piloted flight simulator investigation of a deflected-slipstream VTOL airplane, the Ryan VZ-3RY (National Aeronautics and Space Administration, 1959), by Harry A. James and Ames Research Center (page images at HathiTrust)
• A dynamic model investigation of the effect of a sharp-edge vertical gust on blade periodic flapping angles and bending moments of a two-blade rotor (National Aeronautics and Space Administration, 1959), by John Locke McCarty, Domenic J. Maglieri, George W. Brooks, and Langley Research Center (page images at HathiTrust)
• Effects of body and fin deflections on the aerodynamic characteristics in pitch of a 0.065-scale model of a four-stage rocket configuration at Mach numbers of 1.41 and 1.82 (National Aeronautics and Space Administration, 1959), by Ross B. Robinson and Langley Research Center (page images at HathiTrust)

Items below (if any) are from related and broader terms.