The Online Books Page

Aircraft stability

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

• 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)
• Incipient- and developed-spin and recovery characteristics of a modern high-speed fighter design with low aspect ratio as determined from dynamic-model tests (National Aeronautics and Space Administration, 1961), by Henry A. Lee, Charles E. Libbey, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Analysis of the dynamic lateral stability of a delta-wing airplane with frequency-dependent stability derivatives (National Aeronautics and Space Administration, 1959), by Albert E. Brown, Albert A. Schy, and Langley Research Center (page images at HathiTrust)
• Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by the free-oscillation method (National Aeronautics and Space Administration, 1960), by W. J. Tuovila, R. W. Hess, 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)

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