Thrust augmentation by after-burning in a scramjet nozzle

M. J. Candon, H. Ogawa, G. E. Dorrington

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

A numerical study of scramjet after-burning through the injection of liquid oxygen into the nozzle is conducted. A maximum thrust augmentation of 300% is found. An understanding of the thrust augmentation phenomenon is provided in the form of a force contribution breakdown, analysis of the nozzle flowfields and finally the analysis of the surface pressure and shear stress distributions acting upon the nozzle wall.

本文言語英語
ホスト出版物のタイトルProceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014
出版社Australasian Fluid Mechanics Society
ISBN(電子版)9780646596952
出版ステータス出版済み - 1 1 2014
外部発表はい
イベント19th Australasian Fluid Mechanics Conference, AFMC 2014 - Melbourne, オーストラリア
継続期間: 12 8 201412 11 2014

出版物シリーズ

名前Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014

会議

会議19th Australasian Fluid Mechanics Conference, AFMC 2014
Countryオーストラリア
CityMelbourne
Period12/8/1412/11/14

All Science Journal Classification (ASJC) codes

  • Fluid Flow and Transfer Processes

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