Dynamic Characteristics of Separation Shock in an Unstarted Hypersonic Inlet Flow-Reference-Cited by-同舟云学术

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Dynamic Characteristics of Separation Shock in an Unstarted Hypersonic Inlet Flow

Published:2018-06 Issue:6 Volume:56 Page:2484-2490
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Xue Long-Sheng¹,Wang Cheng-Peng¹,Cheng Ke-Ming¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Funder

National Natural Science Foundation of China

Aeronautical Science Foundation of China

Priority Academic Program Development of Jiangsu Higher Education Institutions

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056660

Reference17 articles.

1. Analysis of possible improvement of acceleration of a high-velocity air-breathing flying vehicle

2. The X-51A Scramjet Engine Flight Demonstration Program

3. Pseudo-shock waves and their interactions in high-speed intakes

4. Recent research progress on unstart mechanism, detection and control of hypersonic inlet

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1. Pressure plateau of separation induced by shock impingement in a Mach 5 flow;Journal of Fluid Mechanics;2023-09-26

2. Oblique shock train motion based on schlieren image processing;Chinese Journal of Aeronautics;2023-03

3. Robust Adaptive Control of Hypersonic Vehicle Considering Inlet Unstart;Journal of Systems Engineering and Electronics;2022-02

4. An integration method based on a novel combined flow for aerodynamic configuration of strutjet engine;Chinese Journal of Aeronautics;2021-09

5. A study on the RR-to-MR transition of shock wave reflections near the leading edge in hypersonic flows;Journal of Fluid Mechanics;2021-06-01

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