Experimental investigation of the turbulent boundary layer at a Mach number of 6 with heat transfer at high Reynolds numbers
By: by Richard D. Samuels, John B. Peterson, Jr., and Jerry B. Adcock
Contributors: Peterson, John B.; Adcock, Jerry B.; Langley Research Center; United States. National Aeronautics and Space Administration
Series: NASA technical note -- NASA TN D-3858; NASA technical note -- D-3858
Publisher: National Aeronautics and Space Administration; For sale by the Clearinghouse for Federal Scientific and Technical Information
Published: 1967
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Number of pages: 73
Subjects: Turbulent boundary layer; Supersonic planes; Design and construction
Notes: "March 1967"--Cover.

Prepared at Langley Research Center.

Includes bibliographical references (p. 16-18).