Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / John W. Edwards.
Saved in:
| Online Access: |
Online Access Online Access |
|---|---|
| Main Author: | |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington, DC] :
[National Aeronautics and Space Administration],
[1996]
|
| Series: | NASA technical memorandum ;
110484. |
| Subjects: |
MARC
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| 100 | 1 | |a Edwards, John W., |e author. |0 http://id.loc.gov/authorities/names/n94033842 | |
| 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. | ||
| 337 | |a computer |b c |2 rdamedia. | ||
| 338 | |a online resource |b cr |2 rdacarrier. | ||
| 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 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration, |e issuing body. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://isni.org/isni/0000000449071619 | |
| 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. |0 http://id.loc.gov/authorities/names/n83707893 | |
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