Longitudinal controlSee also what's at your library, or elsewhere.
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Filed under: Longitudinal control The interpretation of nonlinear pitching moments in relation to the pitch-up problem (National Aeronautics and Space Administration, 1959), by George S. Campbell, Joseph Weil, and Langley Research Center (page images at HathiTrust) A method for longitudinal and lateral range control for a high-drag low-lift vehicle entering the atmosphere of a rotating earth (National Aeronautics and Space Administration, 1961), by John W. Young, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Effects of canard planform and wing-leading-edge modification on low-speed longitudinal aerodynamic characteristics of a canard airplane configuration (National Aeronautics and Space Administration, 1961), by Bernard Spencer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Flight investigations of automatic stabilization of an airplane having static longitudinal instability (National Aeronautics and Space Administration, 1959), by Walter R. Russell, William L. Alford, S. A. Sjoberg, and Langley Research Center (page images at HathiTrust) Flight investigation of an automatic pitchup control (National Aeronautics and Space Administration, 1960), by George J. Hurt, James B. Whitten, and Langley Research Center (page images at HathiTrust) Flight investigation of stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane (National Aeronautics and Space Administration, 1960), by Louis P. Tosti 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) Full-scale wind-tunnel investigation of the longitudinal characteristics of a tilting-rotor convertiplane (National Aeronautics and Space Administration, 1959), by David G. Koenig, Mark W. Kelly, Richard K. Greif, and Ames Research Center (page images at HathiTrust)
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