An experimental study on the spray characteristics of splash platelet injector
Author:
Funder
Hunan Provincial Natural Science Foundation
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference27 articles.
1. B. A. Robbers，b. J. Anderson，w. A. Hayes, et al. Platelet devices-limited only by one’s imagination, 42nd AIAA/ASME/SAE/ASEE Joint Propusion Conference & Exhibit 9-12 July 2006, (Sacramento, California).
2. Investigation on cooling effect with a combinational opposing jet and platelet transpiration concept in hypersonic flow;Shen;Aero. Sci. Technol.,2019
3. Gaseous film cooling investigation in a multi-element splash platelet injector;Yin;Acta Astronaut.,2018
4. Thermal protection characteristics for a combinational opposing jet and platelet transpiration cooling nose-tip;Shen;Acta Astronaut.,2019
5. Numerical investigation on the film cooling performance in a multi-elements splash platelet injector;Yin;Acta Astronaut.,2018
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2. Characteristics of Flow Development and Boiling Transitions in the Liquid Oxygen Chill-Down Process in a Straight Horizontal Exit-Contracted Pipe;International Journal of Aerospace Engineering;2023-02-07
3. Numerical Investigation of the Combustion Characteristics of GO2/GCH4 Splash Platelet Injector;Journal of Aerospace Engineering;2022-07
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