Unsteady flow in a supercritical supersonic diffuser

Author:

Biedron R. T.1,Adamson T. C.1

Affiliation:

1. University of Michigan, Ann Arbor, Michigan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 17 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. Flow Field Investigation of a Rectangular Supersonic Air-Intake With Cowl Bending;Journal of Aerospace Sciences and Technologies;2023-08-07

2. Study on integrated control for supersonic inlet and turbofan engine model;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-07-27

3. Study on Inlet and Engine Integrated Model with Normal Shock Position Feedback;International Journal of Aerospace Engineering;2020-01-04

4. Analytical and numerical study of normal shock response in a uniform duct;Physics of Fluids;2018-08

5. Optimal Terminal Shock Position Under Disturbances for Ramjet Supercritical Operation;Journal of Propulsion and Power;2013-01

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