Numerical Experiment of Aeroelastic Stability for a Rocket Nozzle-Reference-Cited by-同舟云学术

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Numerical Experiment of Aeroelastic Stability for a Rocket Nozzle

Published:2017-09 Issue:5 Volume:30 Page:04017041
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Joanna A.¹,Shotorban Babak²,Zhang Sijun³

Affiliation:

1. Student, Dept. of Mechanical and Aerospace Engineering, Univ. of Alabama in Huntsville, 301 Sparkman Dr., Huntsville, AL 35899.

2. Associate Professor, Dept. of Mechanical and Aerospace Engineering, Univ. of Alabama in Huntsville, 301 Sparkman Dr., Huntsville, AL 35899.

3. Technical Fellow, ESI CFD, Inc., 6767 Old Madison Pike, STE 600, Huntsville, AL 35806 (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000746

Reference17 articles.

1. CFD-FASTRAN V2014.0 [Computer software]. ESI-Group Paris.

2. Frey M. and Hagemann G. (1999). “Flow separation and side loads in rocket nozzles.” 35th Joint Propulsion Conf. and Exhibit AIAA Reston VA.

3. Scalability for Rocket Nozzle Flows Based on Subscale and Full-Scale Testing

4. Numerical validation of a stability model for a flexible over-expanded rocket nozzle

5. A numerical investigation of side-loads resulting from rigid body motions of an overexpanded engine nozzle

Cited by 3 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. Mechanisms Contributing to the Dynamic Stability of a Flexible Subscale Rocket Nozzle;Journal of Propulsion and Power;2024-01

2. Numerical Investigation on Mechanism of External Flow Field–Induced Separation Pattern Transition;Journal of Aerospace Engineering;2023-03

3. Rocket nozzles: 75 years of research and development;Sādhanā;2021-04-11

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