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

Bibliographic Details
Main Author: Edwards, John W. (Author)
Format: Government Document eBook
Language:English
Published: [Washington, DC] : [National Aeronautics and Space Administration], [1996]
Series:NASA technical memorandum ; 110484.
Subjects:
Separated flow.
Transonic flow.
Transonic flutter.
Transonic speed.
Unsteady flow.
Viscous flow.
Computational fluid dynamics.
Coupling.
Airfoils.
Mach number.
Boundary layer separation.
Airfoil oscillations.
Online Access:https://purl.fdlp.gov/GPO/gpo78886

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https://purl.fdlp.gov/GPO/gpo78886

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Call Number: NAS 1.15:110484
 
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NAS 1.15:110484 Available