دورية أكاديمية
Transient spray combustion characteristics in a gas–liquid pintle rocket engine under acoustic excitation.
العنوان: | Transient spray combustion characteristics in a gas–liquid pintle rocket engine under acoustic excitation. |
---|---|
المؤلفون: | Jin, Xuan, Zhu, Chao, Chen, Dejiang, Zhang, Zhongpei |
المصدر: | Scientific Reports; 6/7/2024, Vol. 14 Issue 1, p1-14, 14p |
مصطلحات موضوعية: | ROCKET engines, ACOUSTIC excitation, HEAT of combustion, TEMPERATURE distribution, FIRE testing, SPRAY combustion, SOUND pressure, FLAME temperature |
مستخلص: | In order to investigate the acoustic oscillation characteristics of gas–liquid pintle rocket engines and elucidate the path by which spray combustion process provides energy to the combustor pressure oscillation, a LOX/GCH |
Copyright of Scientific Reports is the property of Springer Nature and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
قاعدة البيانات: | Complementary Index |
كن أول من يترك تعليقا!