An effective approximation for computing the three-dimensional laminar boundary-layer flows
- 1 August 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (8) , 1649-1651
- https://doi.org/10.2514/3.6409
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Similar solutions for the hypersonic laminar boundary layer near a plane of symmetryAIAA Journal, 1965
- Viscous Hypersonic Flow Past a Slender ConePhysics of Fluids, 1964