Aircraft controlSee also what's at your library, or elsewhere.
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Filed under: Aircraft control- A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume III, Propulsion subsystems, performance, stability and control, propellers, and flight safety (National Aeronautics and Space Administration ;, 1970), by Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
- 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)
- 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)
- Measured and theoretical flow fields behind a rectangular and a triangular wing up to high angles of attack at a Mach number of 2.46 (National Aeronautics and Space Administration, 1959), by Frank J. Centolanzi and Ames 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)
- An analog study of an airborne automatic landing-approach system (National Aeronautics and Space Administration, 1959), by James J. Adams and Langley Research Center (page images at HathiTrust)
- A limited flight and wind-tunnel investigation of paddle spoilers as lateral controls (National Aeronautics and Space Administration, 1959), by Robert G. Mungall, William L. Alford, Harold I. Johnson, and Langley Research Center (page images at HathiTrust)
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