The Online Books Page

Books by Byron M. Jaquet:

Books in the extended shelves:

• Jaquet, Byron M.: Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Jaquet, Byron M.: Dynamic stability and dispersion of a Project Mercury test capsule upon entering the atmosphere, with effects of roll rate, center-of-gravity displacement, and threshold of a rate-reaction control system (National Aeronautics and Space Administration, 1961), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Jaquet, Byron M.: Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms (National Advisory Committee for Aeronautics, 1950), also by Alex Goodman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Jaquet, Byron M.: Some low-speed wind-tunnel experiments pertaining to the longitudinal stability characteristics of a 35° swept-wing model and an unswept-wing model (National Advisory Committee for Aeronautics, 1953), also by United States. National Adviosry Committee for Aeronautics and Langley Aeronautical Laboratory (page images at HathiTrust)
• Jaquet, Byron M.: Static longitudinal and lateral stability characteristics at a mach number of 3.11 of square and circular plan-form reentry vehicles, with some effects of controls and leading-edge extensions (National Aeronautics and Space Administration, 1960), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Jaquet, Byron M.: A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results (National Advisory Committee for Aeronautics, 1950), also by John D. Bird and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Jaquet, Byron M.: Wind-tunnel investigation of effects of ventral fins at two positions on lateral-stability derivatives of 45° high-wing model oscillating in yaw (National Advisory Committee for Aeronautics, 1957), also by United States National Advisory Committee for Aeronautics (page images at HathiTrust)

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