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

An edition of Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method (1996)

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

EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996

By Euromech Colloquium (349th 1996 Göttingen, Germany)

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Airfoil oscillations, Airfoils, Boundary layer separation, Computational fluid dynamics, Coupling, Mach number, Separated flow, Transonic flow, Transonic flutter, Transonic speed, Unsteady flow, Viscous flow