The Online Books Page

Books by Jim A. Penland:

Books in the extended shelves:

• Penland, Jim A.: Aeordynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), also by Jimmy L. Pittman and Langley Research Center (page images at HathiTrust)
• Penland, Jim A.: Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by James B. Hallissy, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Penland, Jim A.: Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach number 0.2 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by James L. Dillon, Theodore R. Creel, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Penland, Jim A.: Aerodynamic force characteristics of a series of lifting cone and cone-cylinder configurations at a mach number of 6.83 and angles of attack up to 130⁰ (National Aeronautics and Space Administration :, 1961), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Penland, Jim A.: Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Don C. Marcum and Langley Research Center (page images at HathiTrust)
• Penland, Jim A.: Experimental low-speed and calculated high-speed aerodynamic characteristics of a hypersonic research airplane concept having a 65 ̊swept delta wing (National Aeronautics and Space Administration ;, 1974), also by Floyd G. Howard, Theodore R. Creel, and Langley Research Center (page images at HathiTrust)
• Penland, Jim A.: Lift, drag, and static longitudinal stability data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form (National Advisory Committee for Aeronautics, 1955), also by David E. Fetterman, Herbert W. Ridyard, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Penland, Jim A.: NASA TN D-4122 (National Aeronautics and Space Administration ;, 1967), also by Peter T. Bernot and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Penland, Jim A.: Static longitudinal, directional, and lateral stability and control data at a mach number of 6.83 of the final configuration of the X-15 research airplane (National Aeronautics and Space Administration, 1960), also by Jr. Fetterman and Langley Research Center (page images at HathiTrust)
• Penland, Jim A.: A study of the aerodynamic characteristics of a fixed geometry paraglider configuration and three canopies with simulated variable canopy inflation at a mach number of 6.6 (National Aeronautics and Space Administration :, 1962), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Penland, Jim A.: Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Sharon H. Stack, Don C. Marcum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

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