A shock tube investigation of heat transfer in the wake of a hemisphere-cylinder, with application to hypersonic flight
By: William E. Powers, Kenneth F. Stetson and Mac C. Adams
Contributors: Stetson, Kenneth F.; Adams, Mac C.
Series: Research report (Avco Research Laboratory) -- 30; Research report (Avco-Everett Research Laboratory) -- 30
Publisher: Avco Manufacturing Corp., Avco Research Laboratory
Published: 1958
Place of publication: Everett, Mass.]
Language: eng
Number of pages: 36
Subjects: Hypersonic Aerodynamics; Heat; Transmission; Shock tubes
Notes: "... sponsored by the Ballistic Missile Division, Air Research and Development Command, United States Air Force under Contract AF 04(645)-18."

"August 1958."

Includes bibliographical references (p. [39]).