Preliminary study on the influence of aerothermoelastic deformation on 2-D hypersonic inlet performance-Reference-Cited by-同舟云学术

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Preliminary study on the influence of aerothermoelastic deformation on 2-D hypersonic inlet performance

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
language:
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Author:

Guangyue Dai¹,Zeng Lei¹,Jia Hongyin¹,Liu Lei¹,Qiu Bo¹,Gui Yewei¹

Affiliation:

1. China Aerodynamics Research and Development Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2403

Reference11 articles.

1. 2Martin Krause, Josef Ballmann. Numerical simulations and Design of a scramjet intake using two different RANS solvers[C].43rdAIAA/ASME/SAE/ASEE JointPropulsionConference&Exhibit,8-11 July2007, Cincinnati, OH

Cited by 4 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. Coupling Strategies for Analyzing Fluid-Thermal-Structural Interactions of a Hypersonic Inlet;AIAA SCITECH 2024 Forum;2024-01-04

2. Fully Coupled Analysis of Aerothermoelastic Deformation of a Scramjet Inlet;Journal of Propulsion and Power;2023-10-18

3. Experimental Study of Aeroelastic Response and Performance of a Hypersonic Intake Ramp;Journal of Propulsion and Power;2022-01

4. Experimental Study of the Aeroelastic Response and Performance of a Hypersonic Intake;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10

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