Computational, theoretical, and experimental investigation of flow over a sharp flat plate, M1 = 10 - 25
By: Henry T. Nagamatsu, D. G. Messitt, L. N. Myrabo and R. E. Sheer.
Contributors: Messitt, D. G.; Myrabo, L. N.; Sheer, R. E.; AIAA
Publisher: American Institute of Aeronautics and Astronautics
Published: 1994
Place of publication: Washington, D. C
Number of pages: 14
Subjects: Hypersonic flow; shock-boundary layer interaction
Notes: Includes bibliographical references: p. 7-8.

Source: 25th AIAA Fluid Dynamics Conference, June 20-23, 1994/Colorado Springs, CO