Item Details

Aerodynamic Characteristics of a Swept-Wing Cruise Missile at Mach Numbers From 0.50 to 2.86

by M. Leroy Spearman and Ida K. Collins
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972.
Language
English
Series
NASA Technical Note
Description
40 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
Series Statement
NASA technical note ; NASA TN D-7069
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86 / c| by M. Leroy Spearman and Ida K. Collins.
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    a| Aerodynamics, Transonic.
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    a| Aerodynamics, Supersonic.
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