Investigation of a Wide Range Adaptable Hypersonic Dual-Waverider Integrative Design Method Based on Two Different Types of 3D Inward-Turning Inlets-Reference-Cited by-同舟云学术

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Investigation of a Wide Range Adaptable Hypersonic Dual-Waverider Integrative Design Method Based on Two Different Types of 3D Inward-Turning Inlets

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

Author:

Xianhong Xiang¹,Yuan Liu¹,Qian Zhansen¹

Affiliation:

1. Aviation Industry Corporation of China (AVIC)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2110

Reference19 articles.

1. Lewis MA. Hypersonicpropulsionairframe integrationoverview.AIAA2003-4405.

2. YouYancheng, Zhu Chengxiang, Guo Junliang. Overview of the integration of the three dimensional inward turninghypersonic inletandforebody.2009,39(5):513-525.(inChinese)

3. Walker S.H.,F.Rodgers. Falconhypersonic technologyoverview.AIAA2005-3253.

4. Yancheng You, Chengxiang Zhu, Junliang Guo. Dual waverider concept for the integration of hypersonic inward-turninginletandairframe forebody.AIAA2009-7421.

Cited by 2 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. Investigating the impacts of aerodynamics of wings and body on airplane motion equations;Revista Română de Informatică și Automatică;2020-12-18

2. Modern problems of aircraft aerodynamics;Advances in Aerodynamics;2019-03-07

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