Open AccessCoupling Between a Supersonic Turbulent Boundary Layer and a Flexible Structure
Author(s) -
Abdelkader Frendi
Publication year - 1997
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/2.87
Subject(s) - fuselage , boundary layer , supersonic speed , mach number , turbulence , mechanics , physics , coupling (piping) , choked flow , flow (mathematics) , acoustics , classical mechanics , materials science , structural engineering , engineering , metallurgy
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