Calculation of Compressible Turbulent Boundary Layers on an Infinite Yawed Airfoil
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (3) , 131-132
- https://doi.org/10.2514/3.56958
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Finite-difference analysis of the three-dimensional turbulent boundary layer on a sharp cone at angle of attack in a supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Turbulent Heat Transfer on Blunt-Nosed Bodies in Two-Dimensional and General Three-Dimensional Hypersonic FlowJournal of the Aerospace Sciences, 1960