Aeroelastic Coupling and Side Loads in Rocket Nozzles-Reference-Cited by-同舟云学术

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Aeroelastic Coupling and Side Loads in Rocket Nozzles

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:38th Fluid Dynamics Conference and Exhibit
language:
Short-container-title:

Author:

Zhang Sijun¹,Fuchiwaki T.¹

Affiliation:

1. ESI CFD, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4064

Reference14 articles.

1. 2Zhang, S.J., Meganathan, A., Blosch, E. and Saxena, A. "Development and Validation of Transonic Flutter Prediction methodologyusing CFD-FASTRAN,"AIAA-2007-2015,2007.

2. 3CFD-FASTRAN,TheoryManual,Version2008,ESIGroup,2008.

3. 4Yang,H.Q.andWang,Z.J."InteractionofShockWavewithaFlexibleStructure,"AIAAPaper94-0362,1994.

4. 5Brown,S.A."DisplacementExtrapolationforCFDandCSMAnalysis,"AIAAPaper97-1090,1997.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical Experiment of Aeroelastic Stability for a Rocket Nozzle;Journal of Aerospace Engineering;2017-09

2. Aeroelastic Response of Rocket Nozzles Subected to Combined Thrust and Side Loads;22nd AIAA Computational Fluid Dynamics Conference;2015-06-18

3. Development of an Aeroelastic Modeling Capability for Transient Nozzle Flow Analysis;Journal of Propulsion and Power;2014-11

4. Development of an Aeroelastic Modeling Capability for Transient Nozzle Side Load Analysis;49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2013-07-12

5. Aeroelastic response of rocket nozzles to asymmetric thrust loading;Computers & Fluids;2013-05

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