effect of varying Mach number on crossing, glancing shocks/turbulent boundary-layer interactions
By: K. E. Williams and W. R. Hingst.
Contributors: Hingst, W. R.; AIAA
Publisher: AIAA
Published: 1991
Place of publication: Washington, D. C
Number of pages: 11
Subjects: Shock-boundary layer interaction
Notes: Includes bibliographical references: p. 11.

Source: AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference and Exhibit, June 24-26, 1991/Sacramento, California