Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow
- 1 September 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (9), 1870-1872
- https://doi.org/10.2514/3.6439
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary LayersJournal of Basic Engineering, 1970
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- Three-Dimensional Boundary Layer TheoryPublished by Elsevier ,1956