Turbulent boundary-layer heat transfer and transition measurements for cold-wall conditions at Mach 6.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 958-959
- https://doi.org/10.2514/3.4646
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- The mechanics of non-linear materials with memoryArchive for Rational Mechanics and Analysis, 1957