Viscous effects far downstream in a slowly expanding hypersonic nozzle.
- 1 May 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (5) , 807-815
- https://doi.org/10.2514/3.3550
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Integral equations for viscous hypersonic nozzle flowAIAA Journal, 1964
- VISCOUS COMPRESSIBLE AND INCOMPRESSIBLE FLOW IN SLENDER CHANNELSAIAA Journal, 1963
- Turbulent Boundary Layer Measurements at Mach Numbers from 8 to 10Physics of Fluids, 1959
- A METHOD OF CALCULATING TURBULENT-BOUNDARY-LAYER GROWTH AT HYPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1959