Numerical study on the trajectory of a long-range flexible rocket with large slenderness ratio-Reference-Cited by-同舟云学术

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Numerical study on the trajectory of a long-range flexible rocket with large slenderness ratio

Published:2021-10 Issue: Volume:117 Page:106959
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Yabin,Xu Min,An Xiaomin,Xu Zhongxiang,Xu Wei,Quan Enqian^ORCID

Funder

National Natural Science Foundation of China

Aeronautical Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference64 articles.

1. Development in coupling dynamics of flexible high-speed aircraft;Xu,2016

2. Design and manufacture of unmanned aerial vehicles (UAV) wing structure using composite materials;Grodzki;Mater.wiss. Werkst.tech.,2015

3. C/c-sic composite materials nozzle extension design and investigation for lox/lh_2 rocket engine;Wang,2019

4. Review of studies on aeroelasticity of hypersonic vehicles;Yang;Acta Aeronaut. Astronaut. Sin.,2010

5. The flying-wing concept - chances and risks;Dmitriev,2003

Cited by 1 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. Nonlinear Manifold Learning and Model Reduction for Transonic Flows;AIAA Journal;2023-12

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