Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration-Reference-Cited by-同舟云学术

Aeroelastic stability analysis of a flexible over-expanded rocket nozzle using numerical coupling by the method of transpiration

Published:2015-07 Issue: Volume:56 Page:89-106
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Bekka N.,Sellam M.,Chpoun A.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference30 articles.

1. Problématique des ondes de choc dans les tuyères supersoniques et leur interaction avec la structure;Bekka,2014

2. Bekka, N., Sellam, M., Turbelin, G., Chpoun A., 2011. Fluid–Structure Interaction for a Flexible Overexpanded Rocket Nozzle Using the Aeroelastic Stability Model ISSW 28. Manchester, UK.

3. Blades, E.L., Baker, M., Pray, C.L., Luke, E.A., 2012. Fluid–structure interaction simulations of rocket engine side loads, In: Proceedings of the SIMULIA Customer Conference.

4. CFD-GEOM User Manual, 2003. CFD Research Corporation, V2003.

5. Chapman, D.R., Huehn, D.M., Larson, H.K., 1958. Investigation of Separated Flows in Supersonic and Subsonic Streams with Emphasis on the Effect of Transition. Technical Report NACA TR 1356, NACA.

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