Item Details

Flight-Measured Base Pressure Coefficients for Thick Boundary-Layer Flow Over an Aft-Facing Step for Mach Numbers From 0.4 to 2.5

by Sheryll A. Goecke
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], 1973.
Language
English
Series
NASA Technical Note
Description
31 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at the Flight Research Center, Edwards, Calif.
  • Cover title.
  • Bibliography: p. 14-15.
Series Statement
NASA technical note ; NASA TN D-7202
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Flight-measured base pressure coefficients for thick boundary-layer flow over an aft-facing step for Mach numbers from 0.4 to 2.5 / c| by Sheryll A. Goecke.
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    a| 31 p. : b| ill. ; c| 27 cm.
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    a| Prepared at the Flight Research Center, Edwards, Calif.
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    a| Bibliography: p. 14-15.
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    a| B-70 bomber.
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    a| Boundary layer.
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    a| Drag (Aerodynamics) x| Measurement.
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