The Online Books Page

Online Books by

Jarrett K. Huffman

Books from the extended shelves:

• Huffman, Jarrett K.: Effect of vertical-tail location on the aerodynamic characteristics at subsonic speeds of a close-coupled canard configuration (National Aeronautics and Space Administration ;, 1975), also by Langley Research Center (page images at HathiTrust)
• Huffman, Jarrett K.: Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), also by Sheryll Goecke Powers, Charles H. Fox, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Huffman, Jarrett K.: Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode (National Aeronautics and Space Administration ;, 1974), also by Charlie M. Jackson and Langley Research Center (page images at HathiTrust)
• Huffman, Jarrett K.: Lateral-directional stability characteristics of a wing-fuselage configuration at angles of attack up to 44 ̊ (National Aeronautics and Space Administration ;, 1974), also by William P. Henderson and Langley Research Center (page images at HathiTrust)
• Huffman, Jarrett K.: Leading-edge deflection optimization for a highly swept arrow-wing configuration (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Paul L. Coe, James W. Fenbert, Langely Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Huffman, Jarrett K.: NASA TN D-6344 (National Aeronautics and Space Administration ;, 1971), also by Edwin E. Davenport, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Huffman, Jarrett K.: Subsonic longitudinal and lateral-directional characteristics of a forward-swept-wing fighter configuration at angles of attack up to 47⁰ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), also by Michael J. Mann, Charles H. Fox, and Langley Research Center (page images at HathiTrust)
• Huffman, Jarrett K.: Vortex flap flow reattachment line and subsonic longitudinal aerodynamic data on 50⁰ to 74⁰ delta wings on common fuselage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Neal T. Frink, Thomas D. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Huffman, Jarrett K.: Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds (National Advisory Committee for Aeronautics, 1957), also by Alexander D. Hammond, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

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