Item Details

Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio From 4.00 to 1.74 in Combination With a Body

by John R. Sevier, Jr.
Format
Book; Government Document; Online; EBook
Published
Washington [D.C.] : National Aeronautics and Space Administration, [1960]
Language
English
Series
NASA Technical Memorandum
Description
39 p. : 14 ill. ; 27 cm.
Mode of access: Internet.
Notes
  • "January 1960."
  • Cover title.
  • Includes bibliographical references (p. 12).
Series Statement
NASA technical memorandum ; X-172
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Aerodynamic characteristics at mach numbers of 1.41 and 2.01 of a series of cranked wings ranging in aspect ratio from 4.00 to 1.74 in combination with a body / c| by John R. Sevier, Jr.
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    a| 39 p. : b| 14 ill. ; c| 27 cm.
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    a| "January 1960."
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    a| Includes bibliographical references (p. 12).
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    a| Aerodynamics, Supersonic.
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    a| Airplanes x| Wings, Swept-back.
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    a| Stability of airplanes, Longitudinal.
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