Numerical solutions of the flow field produced by a plane shock wave emerging into a crossflow
By: by Lynn D. Tyler and Glen W. Zumwalt.
Contributors: Zumwalt, Glen Wallace, 1926-; Sandia Corporation. Aerodynamic Research Division.; U.S. Atomic Energy Commission. Sandia Laboratory, Albuquerque, N.M.
Publisher: Sandia Corp., Aerodynamic Research Division
Published: 1967
Place of publication: Albuquerque
Language: eng
Number of pages: 180
Subjects: Shock waves -- Mathematical models.
Notes: "SC-DC-65-1916."

"Research report."

"Embodies the Ph. D. dissertation of Lynn D. Tyler."