More about Victor L. Peterson:
| | Books by Victor L. Peterson: Books in the extended shelves: Peterson, Victor L.: Aerodynamic loads at mach numbers from 0.70 to 2.22 on an airplane model having a wing and canard of triangular plan form and either single or twin vertical tails (National Aeronautics and Space Administration :, 1961), also by Gene P. Menees and United States National Aeronautics and Space Administration (page images at HathiTrust) Peterson, Victor L.: Analysis of the errors associated with the determination of planetary atmosphere structure from measured accelerations of an entry vehicle (National Aeronautics and Space Administration ;, 1965), also by Ames Research Center (page images at HathiTrust) Peterson, Victor L.: Angle-of-attack convergence of spinning bodies entering planetary atmospheres at large inclinations to the flight path (National Aeronautics and Space Administration :, 1964), also by Murray Tobak, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Peterson, Victor L.: Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 (National Aeronautics and Space Administration, 1960), also by Loren G. Bright and Ames Research Center (page images at HathiTrust) Peterson, Victor L.: Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 (National Aeronautics and Space Administration :, 1962), also by Robert L. McKenzie and United States National Aeronautics and Space Administration (page images at HathiTrust) Peterson, Victor L.: Equations for isentropic and plane shock flows of mixtures of undissociated planetary gases (National Aeronautics and Space Administration, 1965) (page images at HathiTrust) Peterson, Victor L.: Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust) Peterson, Victor L.: Static stability and control of canard configurations at mach numbers from 0.70 to 2.22 - trangular wing and canard with twin vertical tails (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust) Peterson, Victor L.: Theory of tumbling bodies entering planetary atmospheres with application to probe vehicles and the Australian tektites (National Aeronautics and Space Administration, 1964), also by Murray Tobak (page images at HathiTrust)
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