Online Books by
Paul G. Fournier
Books from the extended shelves:
- Fournier, Paul G.: Aerodynamic characteristics at low speed of a reentry configuration having rigid retractable conical lifting surfaces. (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: Aerodynamic characteristics of a canard and an outboard-tail airplane model at high subsonic speeds (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: Low-speed aerodynamic characteristics of a transport model having 42.33 ̊swept low wing with supercritical airfoil, double-slotted flaps, and T-tail or low tail (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)
- Fournier, Paul G.: Low-speed effects of high-lift devices on the aerodynamic characteristics of a supersonic transport model with outboard tails (National Aeronautics and Space Administration, 1963), also by William C. Sleeman, Edward J. Ray, and Langley Research Center (page images at HathiTrust)
- Fournier, Paul G.: Low-speed investigation of static longitudinal and lateral stability characteristics of an airplane configuration with a highly tapered wing and with several body and tail arrangements (National Aeronautics and Space Administration, 1960) (page images at HathiTrust)
- Fournier, Paul G.: Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep (National Aeronautics and Space Administration, 1961), also by B. Ann Bell, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
- Fournier, Paul G.: NASA TN D-2030 (National Aeronautics and Space Administration, 1963), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Fournier, Paul G.: NASA TN D-5965 (National Aeronautics and Space Administration :, 1970), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: NASA TN D-5974 (National Aeronautics and Space Administration :, 1970), also by William C. Sleeman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: Pressure distributions on 3 rigid wings simulating parawings with varied canopy curvature and leading-edge sweep at Mach numbers from 2.29 to 4.65 (National Aeronautics and Space Administration, 1963), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
- Fournier, Paul G.: Transonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading edge sweep (National Aeronautics and Space Administration :, 1962), also by B. Ann Bell and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: Wind-tunnel investigation at high subsonic speed of the static longitudinal stability characteristics of a winged reentry vehicle having a large negatively deflected flap-type control surface (National Aeronautics and Space Administration, 1959), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
- Fournier, Paul G.: Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4 (National Advisory Committee for Aeronautics, 1953), also by Langley Aeronautical Laboratory and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
- Fournier, Paul G.: Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. Aspect-ratio series (National Advisory Committee for Aeronautics, 1953), also by Andrew L. Byrnes, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
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