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Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing

โœ Scribed by Ermolaev, Yu. G.; Kolosov, G. L.; Kosinov, A. D.; Semenov, N. V.


Book ID
125392901
Publisher
Springer
Year
2014
Tongue
English
Weight
294 KB
Volume
49
Category
Article
ISSN
0015-4628

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The eects of mean ยฏow three-dimensionality on the turbulent structure of the boundary layer on a swept wing are investigated experimentally. The conยฎguration of the test model used to simulate the inยฎnite swept wing condition is similar to that used by Van den Berg, B., Elsenaar, A., Lindhout, J.P.F