The Online Books Page

Books by Samuel M. Dollyhigh:

Books in the extended shelves:

• Dollyhigh, Samuel M.: Effects of stores on longitudinal aerodynamic characteristics of a fighter at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by William J. Monta, Giuliana Sangiogio, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dollyhigh, Samuel M.: Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dollyhigh, Samuel M.: Experimental effects of fuselage camber on longitudinal aerodynamic characteristics of a series of wing-fuselage configurations at a mach of 1.41 (U.S. National Aeronautics and Space Administration ;, 1976), also by Mary S. Adams, Odell A. Morris, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Dollyhigh, Samuel M.: Longitudinal aerodynamic characteristics at Mach 0.60 to 2.86 of a fighter configuration with strut braced wing (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Giuliana Sangiorgio, William J. Monta, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dollyhigh, Samuel M.: Static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations at Mach numbers from 1.60 to 2.86. (National Aeronautics and Space Administration :, 1971), also by Langley Research Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Dollyhigh, Samuel M.: Subsonic and supersonic longitudinal stability and control characteristics of an aft-tail fighter configuration with cambered and uncambered wings and cambered fuselage (National Aeronautics and Space Administration ;, 1977), also by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Dollyhigh, Samuel M.: Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage (National Aeronautics and Space Administration ;, 1974), also by Langley Research Center (page images at HathiTrust)
• Dollyhigh, Samuel M.: Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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