Boundary layer induced pressures on a flat plate in unsteady hypersonic flight
- 19 January 1970
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 1953