Online Books by
Gerald V. Foster
Books from the extended shelves:
- Foster, Gerald V.: Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 degree (National Aeronautics and Space Administration, 1960), also by Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Aerodynamic characteristics of a tailless fixed-wing supersonic transport configuration at Mach number 2.20 (National Aeronautics and Space Administration, 1964), also by William A. Corlett and Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Effect of longitudinal and lateral controls on winged reentry configuration at mach 1.97 and angles of attack up to 90° (National Aeronautics and Space Administration, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° (National Aeronautics and Space Administration, 1960), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Exploratory investigation at mach number of 2.01 of the longitudinal stability and control characteristics of a winged reentry configuration (National Aeronautics and Space Administration, 1959), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01 (National Aeronautics and Space Administration, 1959), also by Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Stability and control characteristics at a Mach number of 1.97 of an airplane configuration having two types of variable- sweep wings (National Aeronautics and Space Administration, 1960), also by Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75° (National Aeronautics and Space Administration, 1959), also by M. Leroy Spearman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Stability and control characteristics at mach numbers of 2.50, 3.00, and 3.71 of a variable- wing-sweep configuration with outboard wing panels swept back 75 degree (National Aeronautics and Space Administration, 1960), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors (National Aeronautics and Space Administration, 1963), also by Dennis E. Fuller and Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.01 of a tailless delta V/STOL configuration having variable-sweep wing panels (National Aeronautics and Space Administration, 1961), also by M. Leroy Spearman and Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V/STOL airplane configuration with a variable-sweep wing and with a skewed wing design (National Aeronautics and Space Administration, 1961), also by Odell A. Morris and Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration (National Aeronautics and Space Administration, 1960), also by Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Foster, Gerald V.: Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces (National Aeronautics and Space Administration, 1961), also by Ross B. Robinson and Langley Research Center (page images at HathiTrust)
- Foster, Gerald V.: Static stability characteristics of a series of hypersonic boost-glide configurations at mach numbers of 1.41 and 2.01 (National Aeronautics and Space Administration, 1959), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
See also what's at your library, or elsewhere.
Help with reading books -- Report a bad link -- Suggest a new listing
Home -- Search -- New Listings -- Authors -- Titles -- Subjects -- Serials
Books -- News -- Features -- Archives -- The Inside Story
Edited by John Mark Ockerbloom (onlinebooks@pobox.upenn.edu)
OBP copyrights and licenses.