|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910705776803321 |
|
|
Autore |
Edwards John W. |
|
|
Titolo |
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / / John W. Edwards |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
[Washington, DC] : , : [National Aeronautics and Space Administration], , [1996] |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (16 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Separated flow |
Transonic flow |
Transonic flutter |
Transonic speed |
Unsteady flow |
Viscous flow |
Computational fluid dynamics |
Coupling |
Airfoils |
Mach number |
Boundary layer separation |
Airfoil oscillations |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996." |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (pages 15-16). |
|
|
|
|
|