Development of an Aeroelastic Modeling Capability for Transient Nozzle Flow Analysis-Reference-Cited by-同舟云学术

Development of an Aeroelastic Modeling Capability for Transient Nozzle Flow Analysis

Published:2014-11 Issue:6 Volume:30 Page:1692-1700
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Wang Ten-See¹,Zhao Xiang²,Zhang Sijun³,Chen Yen-Sen⁴

Affiliation:

1. ER42, Fluid Dynamics Branch, Propulsion Structure, Thermal, and Fluids Analysis Division, NASA Marshall Space Flight Center, Huntsville, Alabama 35812

2. Alabama A&M University, Huntsville, Alabama 35762

3. ESI CFD, Inc., Huntsville, Alabama 35806

4. Applied Research Laboratory, Hsinchu 30078, Taiwan, Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35277

Reference36 articles.

1. Sea level side loads in high-area-ratio rocket engines

2. Characteristics of Space Shuttle Main Engine failures

3. LE-7A Engine Nozzle Problems during Transient Operations

4. Rocket Engine Nozzle Side Load Transient Analysis Methodology- a Practical Approach

5. Three Dimensional Unsteady Flow Simulation of Compressed Truncated Perfect Nozzles

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