Viscous and Leading-Edge Thickness Effects on the Pressures on the Surface of a Flat Plate in Hypersonic Flow
- 1 June 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (6) , 430-431
- https://doi.org/10.2514/8.3069
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate SolutionsJournal of the Aeronautical Sciences, 1953
- Results of Recent Hypersonic and Unsteady Flow Research at the Langley Aeronautical LaboratoryJournal of Applied Physics, 1950
- An Analysis of the Mechanics of Metal CuttingJournal of Applied Physics, 1949