Aerodynamic investigation of the shock train in a scramjet with the effects of backpressure and divergent angles-Reference-Cited by-同舟云学术

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Aerodynamic investigation of the shock train in a scramjet with the effects of backpressure and divergent angles

Published:2020-07-13 Issue:8 Volume:49 Page:4857-4869
ISSN:2688-4534
Container-title:Heat Transfer
language:en
Short-container-title:Heat Transfer

Author:

Gugulothu Santhosh K.¹^ORCID

Affiliation:

1. Department of Mechanical Engineering National Institute of Technology Andhra Pradesh Tadepalligudem Andhra Pradesh India

Publisher

Wiley

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/htj.21856

Reference35 articles.

1. Experimental investigation of mechanism and limits for shock train rapid forward movement;Xu K;Exp Therm Fluid Sci,2018

2. Mechanism of shock train rapid motion induced by variation of attack angle;Xu K;Acta Astronaut,2017

3. Transient behavior of shock train with and without controlling;Chen Z;Exp Therm Fluid Sci,2015

4. Numerical investigation on the shock wave transition in a three‐dimensional scramjet isolator;Huang W;Acta Astronaut,2011

5. Aerodynamic performance analysis of a hypersonic inlet isolator using computation and experiment;Reinartz BU;J Propul Power,2003

Cited by 4 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. Potential for Closed-Loop Control of Dual-Mode Scramjets Using Optical Sensors;AIAA Journal;2023-11-29

2. Mechanism of shock-train/boundary-layer interaction in spanwise concave isolator channels;Acta Astronautica;2022-10

3. Numerical analysis of supersonic combustion of hydrogen flow characteristics in scramjet combustor toward the improvement of combustion efficiency;International Journal of Hydrogen Energy;2022-10

4. Numerical investigations on the performance of a multistrut hydrogen injector in a scramjet combustor;Heat Transfer;2021-07-05

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