Start Limits and Positive Control of RBCC Inlet-Reference-Cited by-同舟云学术

Start Limits and Positive Control of RBCC Inlet

Published:2022-03 Issue:2 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Shi Lei¹^ORCID,Yang Yiyan²,Yang Xue²,Zhao Guojun²,Chen Fuhao²,He Guoqiang³

Affiliation:

1. Associate Professor, Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, PR China (corresponding author). ORCID: .

2. Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, PR China.

3. Professor, Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical Univ., Xi’an, Shaanxi 710072, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001382

Reference41 articles.

1. Fifty years of hypersonics: where we've been, where we're going

2. Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight

3. Bulman M. and A. Siebenhaar. 2011. “Combined cycle propulsion: Aerojet innovations for practical hypersonic vehicles.” In Proc. 17th AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf. 2397. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2011-2397.

4. Unstart margin control of hypersonic inlets

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

Cited by 5 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. Effects of excess oxidizer coefficient on RBCC engine performance in ejector mode: A theoretical investigation;Energy;2024-02

2. The Influence of External Flow Field on the Flow Separation of Overexpanded Single-Expansion Ramp Nozzle;Aerospace;2023-11-13

3. Combustion mode and heat release characteristics of a kerosene-fueled rocket-aided ramjet combustor in ramjet-to-scramjet mode transition;Aerospace Science and Technology;2023-10

4. Numerical Investigation on Mechanism of External Flow Field–Induced Separation Pattern Transition;Journal of Aerospace Engineering;2023-03

5. Schlieren depiction on flow characteristics and dynamic evolution of RBCC inlet under the combined impact of rocket jet and back pressure;Aerospace Science and Technology;2022-12