Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method /
Saved in:
Author / Creator: | Edwards, John W., author. |
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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: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/11288195 |
Other authors / contributors: | United States. National Aeronautics and Space Administration, issuing body. |
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Notes: | "EUROMECH-ColIoquium 349 Simulation of Fluid-Structure Interaction in Aeronautics, Gottingen, Germany, September 16-18, 1996." Includes bibliographical references (pages 15-16). Description based on online resource; title from PDF title page (NASA, viewed June 14, 2017). |
Other form: | Microfiche version: Euromech Colloquium (349th : 1996 : Göttingen, Germany). Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method |
GPO item no.: | 0830-D (online) |
Govt.docs classification: | NAS 1.15:110484 |
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