About this scholarly article

30th Aerospace Sciences Meeting and Exhibit - The hypersonic shock wave-turbulent boundary layer interaction generated by a sharp fin at Mach 8.2 by KNIGHT, DOYLE; HORSTMAN, C.; MONSON, D. is a scholarly article available to read on EtoBox.

Author

KNIGHT, DOYLE; HORSTMAN, C.; MONSON, D.

Publisher

American Institute of Aeronautics and Astronautics

Published

1992