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The Institute of Theoretical and Applied Mechanics
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Original version of the author's contribution as presented on CD, XMLout( page 1005, code PO.FM07-1.11.127).:
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Nonlinear disturbance evolution in supersonic boundary layers on the swept wing
Panina, Alexandra
The paper presented the results on the generation and development of the wave train in uniform and spanwise modulated boundary layer at Mach 2. A swept-wing model was use [...]
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