A theoretical analysis of the driver-reservoir method of driving hypersonic shock tunnels
By: Robert F. Flagg
Contributors: Aerospace Research Laboratories (U.S.)
Series: ARL -- 66-0051
Publisher: Aerospace Research Laboratories, Office of Aerospace Research, United States Air Force
Published: 1966
Place of publication: Wright-Patterson Air Force Base, Ohio
Language: eng
Number of pages: 32
Subjects: Shock tunnels; Shock tubes; Nozzles; Fluid dynamics; Hypersonic Aerodynamics; Mathematical models
Notes: "March 1966"

"Contract ARL-AF 33(615)-2766; project 7065."

Includes bibliographical references (p. 15).