Item Details

Boundary-Layer Transition and Displacement-Thickness Effects on Zero-Lift Drag of a Series of Power-Law Bodies at Mach 6

by George C. Ashby, Jr., and Julius E. Harris
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], 1974.
Language
English
Series
NASA Technical Note
Description
64 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 14-15).
Series Statement
NASA technical note ; NASA TN D-7723
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Includes bibliographical references (p. 14-15).
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    a| Aerodynamic load x| Computer simulation.
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    a| Aerodynamics, Hypersonic x| Computer simulation.
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