Investigation on aeroelastic response of a hypersonic wind tunnel experiment model
Abstract eng: A coupling numerical simulation technology which combined computational fluid dynamics (CFD) method with computational structure dynamic (CSD) is developed. Several kinds of mode to exchange data for CFD/CSD coupled computation is designed. Aeroelastic response of hypersonic wing under Ma 5 wind tunnel experimental condition is calculated as an example. The coupling of bending and torsion mode is captured. The computed result indicates that CFD/CSD method of aeroelastic simulation is feasible and credible.
Publisher:
International Union of Theoretical and Applied Mechanics, 2016
Conference Title:
Conference Title:
24th International Congress of Theoretical and Applied Mechanics
Conference Venue:
Montreal (CA)
Conference Dates:
2016-08-21 / 2016-08-26
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2016-11-15, last modified 2016-11-15
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