Item Details

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-Body-Tail Model at Mach Numbers 1.57, 2.16, and 2.87

by Royce L. McKinney and Lloyd S. Jernell
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:X-1065
Description
44 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • "March 1965."
  • Cover title.
  • Includes bibliographical references (p. 9).
Series Statement
NASA technical memorandum ; X-1065
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Effects of wing planform on the aerodynamic characteristics of a wing-body-tail model at Mach numbers 1.57, 2.16, and 2.87 / c| by Royce L. McKinney and Lloyd S. Jernell.
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    a| Mach number.
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    a| Stability of airplanes, Longitudinal.
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    a| Aerodynamic measurements.
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