AN INTEGRAL METHOD FOR CALCULATION OF SUPERSONIC LAMINAR BOUNDARY LAYER WITH HEAT TRANSFER ON YAWED CONE
- 1 March 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (3), 672-675
- https://doi.org/10.2514/3.1611