Back-Pressure Effects on the Hypersonic Inlet-Isolator Pseudoshock Motions-Reference-Cited by-同舟云学术

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Back-Pressure Effects on the Hypersonic Inlet-Isolator Pseudoshock Motions

Published:2013-11 Issue:6 Volume:29 Page:1391-1399
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Su Wei-Yi¹,Zhang Kun-Yuan¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34803

Reference21 articles.

1. WeitingA. R. “Exploratory Study of Transient Unstart Phenomena in a Three-Dimensional Fixed-Geometry Scramjet Engine,” NASA TN-D-8156, 1976.

2. PIV Measurements of the Unstart Process in a Supersonic Inlet/Isolator

3. Unstart Detection in a Simplified-Geometry Hypersonic Inlet-Isolator Flow

4. Experimental Investigation of Unstart in an Inlet/Isolator Model in Mach 5 Flow

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3. Machine Learning-Based Backpressure Unstart Prediction and Warning Method for Combined Cycle Engine Hypersonic Inlet-Oriented Wide Speed Range;International Journal of Aerospace Engineering;2024-02-29

4. Aerodynamic Instabilities in High-Speed Air Intakes and Their Role in Propulsion System Integration;Aerospace;2024-01-12

5. Computational investigations of the effects of wall surface temperature on a hypersonic inlet isolator;Thermal Science;2024

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