Effects of flexible panels on normal shock trains and performance of scramjet isolators
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference43 articles.
1. Progress and prospects on aeroelasticity of hypersonic vehicles;Ye;Acta Aerodyn. Sin.,2018
2. Unstart phenomena induced by flow choking in scramjet inlet-isolators;kyun Im;Prog. Aerosp. Sci.,2018
3. Supersonic combustion in air-breathing propulsion systems for hypersonic flight;Urzay;Annu. Rev. Fluid Mech.,2018
4. Influences of wall vibration on shock train structures and performance of two-dimensional rectangular isolators in scramjet engine;Meng;Acta Astronaut.,2020
5. Behavior and flow mechanism of shock train self-excited oscillation influenced by background waves;Hou;Acta Astronaut.,2020
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1. Fluid–Structure Interactions between Oblique Shock Trains and Thin-Walled Structures in Isolators;Aerospace;2024-06-18
2. Mechanism of characteristic change of panel flutter caused by oblique shock impingement;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-08-18
3. Experimental and numerical simulation of shock train characteristics in an isolator with incident shocks;Aerospace Science and Technology;2023-07
4. Oscillatory behaviors of multiple shock waves to upstream disturbances;Physics of Fluids;2023-05-01
5. Characteristics of self-excited shock wave oscillations in a supersonic isolator with exit duct configurations;Acta Astronautica;2023-02
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