Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data
By: Sheryll Goecke Powers
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Series: NASA technical memorandum ; 72855
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Office
Published: 1978
Place of publication: [Washington]; Springfield, Va
Language: eng
Number of pages: 35
Subjects: Drag (Aerodynamics); Skin friction (Aerodynamics); Turbulent boundary layer
Notes: Issued May 1978

Includes bibliographical references