Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /
Saved in:
| 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 |
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| 100 | 1 | |a Edwards, John W., |e author. |0 http://id.loc.gov/authorities/names/n94033842 |1 http://viaf.org/viaf/317138961 | |
| 245 | 1 | 0 | |a Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / |c John W. Edwards. |
| 264 | 1 | |a [Washington, DC] : |b [National Aeronautics and Space Administration], |c [1996] | |
| 300 | |a 1 online resource (16 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a NASA-TM ; |v 110484 | |
| 500 | |a "EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996." | ||
| 504 | |a Includes bibliographical references (pages 15-16). | ||
| 588 | |a Description based on online resource; title from PDF title page (NASA, viewed June 14, 2017). | ||
| 650 | 7 | |a Separated flow. |2 nasat | |
| 650 | 7 | |a Transonic flow. |2 nasat | |
| 650 | 7 | |a Transonic flutter. |2 nasat | |
| 650 | 7 | |a Transonic speed. |2 nasat | |
| 650 | 7 | |a Unsteady flow. |2 nasat | |
| 650 | 7 | |a Viscous flow. |2 nasat | |
| 650 | 7 | |a Computational fluid dynamics. |2 nasat | |
| 650 | 7 | |a Coupling. |2 nasat | |
| 650 | 7 | |a Airfoils. |2 nasat | |
| 650 | 7 | |a Mach number. |2 nasat | |
| 650 | 7 | |a Boundary layer separation. |2 nasat | |
| 650 | 7 | |a Airfoil oscillations. |2 nasat | |
| 650 | 7 | |a Aerofoils. |2 fast |0 http://id.worldcat.org/fast/fst00798241 | |
| 650 | 7 | |a Computational fluid dynamics. |2 fast |0 http://id.worldcat.org/fast/fst01745072 | |
| 650 | 7 | |a Mach number. |2 fast |0 http://id.worldcat.org/fast/fst01004756 | |
| 650 | 7 | |a Viscous flow. |2 fast |0 http://id.worldcat.org/fast/fst01167826 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e issuing body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 776 | 0 | 8 | |i Microfiche version: |a Euromech Colloquium (349th : 1996 : Göttingen, Germany). |t Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method |w (OCoLC)42671384 |
| 830 | 0 | |a NASA technical memorandum ; |v 110484. | |
| 856 | 4 | 0 | |u http://purl.fdlp.gov/GPO/gpo78886 |y GPO Documents Without Shelves |
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