Effects of trips on the oscillatory flow of an axisymmetric hypersonic inlet with downstream throttle-Reference-Cited by-同舟云学术

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Effects of trips on the oscillatory flow of an axisymmetric hypersonic inlet with downstream throttle

Published:2018-02 Issue:2 Volume:31 Page:225-236
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

GAO Wenzhi,LI Zhufei,YANG Jiming,ZENG Yishan

Funder

China Postdoctoral Science Foundation

Fundamental Research Funds for the Central Universities of China

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference25 articles.

1. Scramjet inlets;Van Wie,2000

2. Experimental investigation of unstart in an inlet/isolator model in Mach 5 flow;Wagner;AIAA J,2009

3. Experimental investigation of the unstart process of a generic hypersonic inlet;Tan;AIAA J,2011

4. Unsteady behaviors of a hypersonic inlet caused by throttling in shock tunnel;Li;AIAA J,2013

5. Unstart phenomena induced by mass addition and heat release in a model scramjet;Im;J Fluid Mech,2016

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

3. A review of the shock-dominated flow in a hypersonic inlet/isolator;Progress in Aerospace Sciences;2023-11

4. Mitigating Forced Shock-Wave Oscillation with Two-Dimensional Wavy Surface;Aerospace;2022-11-26

5. Assessing the Performance of Hypersonic Inlets by Applying a Heat Source with the Throttling Effect;Aerospace;2022-08-16

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