Novel design methodology of integrated waverider with drip-like intake based on planform leading-edge definition method-Reference-Cited by-同舟云学术

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Novel design methodology of integrated waverider with drip-like intake based on planform leading-edge definition method

Published:2020-02 Issue: Volume:167 Page:314-330
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Chen Shao-Hua,Liu Jun,Ding Feng,Huang Wei

Funder

National Natural Science Foundation of China

Natural Science Foundation of Hunan Province of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. An Aerodynamic Analysis of the Generic Hypersonic Vehicle, AIAA Paper 2018-0637;Ferguson,2018

2. An overview of waverider design concept in airframe/inlet integration methodology for air-breathing hypersonic vehicles;Ding;Acta Astronaut.,2018

3. Novel osculating flowfield methodology for hypersonic waverider vehicles based on variable shock angle;Liu;J. Aerosp. Eng.,2018

4. High-pressure capturing wing configurations;Cui;AIAA J.,2017

5. Hypersonic I-shaped aerodynamic configurations;Cui;Sci. China (Phys., Mech. Astron.),2018

Cited by 10 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. Waverider Design Using Osculating Method;AIAA Journal;2024-05

2. Evaluation of the Pressure-Corrected Osculating Axisymmetric Flows Method for Designing Hypersonic Wavecatcher Intakes with Shape Transition;Journal of Aerospace Engineering;2024-05

3. Aerodynamic analysis of an airframe-inlet integrated full-waverider vehicle designed by osculating cone theory;Acta Astronautica;2024-01

4. Upgraded design methodology for airframe/engine integrated full-waverider vehicle considering thrust chamber design;Acta Astronautica;2023-10

5. Effects of non-uniform inflow to side- and central- spillage bump inlets;AIAA AVIATION 2023 Forum;2023-06-08

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