Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method View on Open Library

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

by Euromech Colloquium (349th 1996 Göttingen, Germany)

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First published: 1996 1 language
Subjects
Airfoil oscillations Airfoils Boundary layer separation Computational fluid dynamics Coupling Mach number Separated flow Transonic flow Transonic flutter Transonic speed

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