Numerical study on the morphology of a liquid-liquid pintle injector element primary breakup spray
Author:
Funder
National Natural Science Foundation of China
Publisher
Zhejiang University Press
Subject
General Engineering
Link
https://link.springer.com/content/pdf/10.1631/jzus.A1900624.pdf
Reference18 articles.
1. Cheng P, Li QL, Xu S, 2017. On the prediction of spray angle of liquid-liquid pintle injectors. Acta Astronautica, 138: 145–151. https://doi.org/10.1016/j.actaastro.2017.05.037
2. Cheng P, Li QL, Chen HY, 2019. Flow characteristics of a pintle injector element. Acta Astronautica, 154:61–66. https://doi.org/10.1016/j.actaastro.2018.10.020
3. Dombrowski N, 1963. The aerodynamic instability and disintegration of viscous liquid sheets. Chemical Engineering Science, 18:203–214. https://doi.org/10.1016/0009-2509(63)85005-8
4. Dressler GA, 2000. TRW pintle engine heritage and performance characteristics. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Article 2000-3871. https://doi.org/10.2514/6.2000-3871
5. Dressler GA, 2006. Summary of deep throttling rocket engines with emphasis on Apollo LMDE. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Article 2006-5220. https://doi.org/10.2514/6.2006-5220
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