Boundary layer suction timing and location effects on unstarting flows in a model scramjet-Reference-Cited by-同舟云学术

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Boundary layer suction timing and location effects on unstarting flows in a model scramjet

Published:2023-09 Issue: Volume:140 Page:108454
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hwang Jeongjae,Im Seong-kyun

Funder

Defense Acquisition Program Administration

Korea Aerospace Research Institute

Agency for Defense Development

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference64 articles.

1. Hypersonic Airbreathing Propulsion;Heiser,1994

2. Scramjet engines: the first forty years;Curran;J. Propuls. Power,2001

3. The Scramjet Engine: Processes and Characteristics;Segal,2009

4. Exploratory study of transient unstart phenomena in a three-dimensional fixed-geometry scramjet engine;Wieting,1976

5. Two-dimensional generic inlet unstart detection at Mach 2.5–5.0;Hawkins,1995

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1. Impact of energy deposition as active flow control on scramjet inlet performance using Immersed Boundary Method;Acta Astronautica;2024-11

2. Influence of fluidic shock control on the combustion flow field of a dual-mode scramjet;Aerospace Science and Technology;2024-07

3. Numerical study of a scramjet isolator performance under different sidewall compression angles;Thermal Science and Engineering Progress;2023-12

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