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: Adams, Mac C.; Stetson, Kenneth F.; Institute of the Aeronautical Sciences (U.S.)
Series: Institute of the Aeronautical Sciences. Report -- no. 59-35
Publisher: Institute of the Aeronautical Sciences
Published: 1959
Place of publication: New York
Number of pages: 24
Notes: Bibliography: p. 23-24.

Source: Presented at the IAS 27th Annual Meeting, New York, N.Y., January 26-29, 1959