Conjugate thermal analysis of X-51A-like aircraft with regenerative cooling channels-Reference-Cited by-同舟云学术

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Conjugate thermal analysis of X-51A-like aircraft with regenerative cooling channels

Published:2022-07 Issue: Volume:126 Page:107614
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Han Dabin^ORCID,Kim Jae Seung^ORCID,Kim Kyu Hong^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Scramjet engines enabling the seamless integration of air & space operations;Andreadis;Ind. Phys.,2004

2. Hypersonic Airbreathing Propulsion;Heiser,1994

3. Advances in hot structure development;Rivers,2006

4. Effects of thermally cracked component of n-dodecane on supersonic combustion behaviors in a scramjet model combustor;Nakaya;Combust. Flame,2015

5. X-51 development: a chief engineer's perspective;Mutzman,2011

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1. Experimental study of CO2 heat transfer at supercritical pressure in combined passages of parallel rectangular channels and porous media channels under supersonic mainstreams;Applied Thermal Engineering;2024-11

2. Numerical investigation of the thermal-mechanical behaviors in the regenerative cooling channel considering thermal pyrolysis;International Communications in Heat and Mass Transfer;2024-09

3. Real-time reconstruction of 3D transient non-uniform temperature field for thermal protection system based on machine learning;Aerospace Science and Technology;2024-08

4. Flow and heat transfer characteristics of hydrocarbon fuel in lightweight C/SiC regenerative cooling combustor;Aerospace Science and Technology;2024-08

5. Verification and characteristics of continuous rotating detonation waves in a novel rounded-rectangle hollow combustor;Physics of Fluids;2024-06-01

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