Thrust augmentation by after-burning in a scramjet nozzle
Publication
, Conference
Candon, MJ; Ogawa, H; Dorrington, GE
Published in: Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014
January 1, 2014
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.
Duke Scholars
Published In
Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014
Publication Date
January 1, 2014
Citation
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ICMJE
MLA
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Candon, M. J., Ogawa, H., & Dorrington, G. E. (2014). Thrust augmentation by after-burning in a scramjet nozzle. In Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014.
Candon, M. J., H. Ogawa, and G. E. Dorrington. “Thrust augmentation by after-burning in a scramjet nozzle.” In Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014, 2014.
Candon MJ, Ogawa H, Dorrington GE. Thrust augmentation by after-burning in a scramjet nozzle. In: Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014. 2014.
Candon, M. J., et al. “Thrust augmentation by after-burning in a scramjet nozzle.” Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014, 2014.
Candon MJ, Ogawa H, Dorrington GE. Thrust augmentation by after-burning in a scramjet nozzle. Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014. 2014.
Published In
Proceedings of the 19th Australasian Fluid Mechanics Conference Afmc 2014
Publication Date
January 1, 2014