Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /
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| Author / Creator: | Edwards, John W., author. |
|---|---|
| Imprint: | [Washington, DC] : [National Aeronautics and Space Administration], [1996] |
| Description: | 1 online resource (16 pages) : illustrations. |
| Language: | English |
| Series: | NASA-TM ; 110484 NASA technical memorandum ; 110484. |
| Subject: | Separated flow. Transonic flow. Transonic flutter. Transonic speed. Unsteady flow. Viscous flow. Computational fluid dynamics. Coupling. Airfoils. Mach number. Boundary layer separation. Airfoil oscillations. Aerofoils. Computational fluid dynamics. Mach number. Viscous flow. |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/11288195 |