The Online Books Page

Books by Roger H. Fournier:

Books in the extended shelves:

• Fournier, Roger H.: Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hull-type airplane with a variable-incidence wing (National Aeronautics and Space Administration, 1960), also by William W. Petynia, Albin O. Pearson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fournier, Roger H.: Aerodynamic characteristics in pitch of a 1/7-scale model of a two- and three-stage rocket configuration at Mach numbers of 0.4 to 4.63 (National Aeronautics and Space Administration ;, 1969), also by William F. Hinson, Richard A. Langhans, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Fournier, Roger H.: Aerodynamic characteristics of a 60 degree sweptback-wing airplane configuration having tail surfaces located outboard of the wingtips at mach numbers of 2.30, 2.97, 3.51, and 4.06 (National Aeronautics and Space Administration, 1960), also by Jr. Sleeman, James D. Church, and Langley Research Center (page images at HathiTrust)
• Fournier, Roger H.: Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Barrett L. Shrout, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Informaton Office (page images at HathiTrust)
• Fournier, Roger H.: Investigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 (National Advisory Committee for Aeronautics, 1958), also by H. Norman Silvers, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Fournier, Roger H.: NASA TN D-2352 (National Aeronautics and Space Administration :, 1964), also by Dennis E. Fuller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fournier, Roger H.: Stability and control characteristics at Mach numbers from 0.20 to 4.63 of a cruciform air-to-air missile with triangular canard controls and a trapezoidal wing (National Aeronautics and Space Administration ;, 1974), also by Ernald B. Graves and Langley Research Center (page images at HathiTrust)
• Fournier, Roger H.: Static aerodynamic characeristics of a winged single-stage-to-orbit vehicle at Mach numbers from 0.3 to 4.63 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Delma C. Freeman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Fournier, Roger H.: Static aerodynamic characteristics of a 1/9-scale model of the escape and exit configurations of the Project Mercury spacecraft at Mach numbers from 2.30 to 4.65 (National Aeronautics and Space Administration, 1962), also by Langley Research Center (page images at HathiTrust)
• Fournier, Roger H.: Static aerodynamic characteristics of a single-stage-to-orbit vehicle with low planform loading at Mach numbers from 0.3 to 4.63 (Scientific and Techn. Information Off., NASA, 1977), also by Delma C. Freeman (page images at HathiTrust)
• Fournier, Roger H.: Supersonic aerodynamic characteristics of a Saturn IB launch vehicle model with third-stage modifications (National Aeronautics and Space Administration ;, 1966), also by Langley Research Center (page images at HathiTrust)
• Fournier, Roger H.: Supersonic aerodynamic characteristics of a series of wrap-around-fin missile configurations (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)

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