Investigation of hypersonic inlet pulse-starting characteristics at high Mach number-Reference-Cited by-同舟云学术

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Investigation of hypersonic inlet pulse-starting characteristics at high Mach number

Published:2016-11 Issue: Volume:58 Page:427-436
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Jiao Xiaoliang,Chang Juntao^ORCID,Wang Zhongqi,Yu Daren

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Airbreathing hypersonic technology vision vehicles and development dreams;McClinton,1999

2. Preliminary investigation of supersonic diffusers;Kantrowitz,1945

3. Starting characteristics of supersonic inlets;Van Wie,1996

4. Limiting contractions for starting simple Ramp-type scramjet intakes with overboard spillage;Veillard;J. Propuls. Power,2008

5. Numerical investigation of 2-D hypersonic inlet starting characteristic caused by dynamic angle-of-attack;Liu,2010

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1. Experimental research on the flow mechanism of dual-separation unstart phenomenon in hypersonic inlet;Aerospace Science and Technology;2024-07

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

3. UNSTEADY AND QUASI-STEADY MODES OF THE FLOW OVER AN INTAKE TESTED IN A HOTSHOT WIND TUNNEL;Journal of Applied Mechanics and Technical Physics;2023-10

4. Self-Start Characteristics of Hypersonic Inlet When Multiple Unstart Modes Exist;Applied Sciences;2023-08-29

5. Reduced-order-modeling of the transient starting in supersonic passages;Aerospace Science and Technology;2023-08

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