Amplified Laminar Boundary Layer Oscillations and Transition at the Front Attachment Line of a 45° Swept Flat-Nosed Wing with and without Boundary Layer Suction
- 1 January 1969
- book chapter
- Published by Springer Nature
Abstract
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This publication has 1 reference indexed in Scilit:
- On the stability of three-dimensional boundary layers with application to the flow due to a rotating diskPhilosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences, 1955