Thrust augmentation by after-burning in a scramjet nozzle

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

Thrust augmentation by after-burning in a scramjet nozzle

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

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

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.

Original language	English
Title of host publication	Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014
Publisher	Australasian Fluid Mechanics Society
ISBN (Electronic)	9780646596952
Publication status	Published - Jan 1 2014
Externally published	Yes
Event	19th Australasian Fluid Mechanics Conference, AFMC 2014 - Melbourne, Australia Duration: Dec 8 2014 → Dec 11 2014

Publication series

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

Conference

Conference	19th Australasian Fluid Mechanics Conference, AFMC 2014
Country/Territory	Australia
City	Melbourne
Period	12/8/14 → 12/11/14

All Science Journal Classification (ASJC) codes

Fluid Flow and Transfer Processes

Cite this

Thrust augmentation by after-burning in a scramjet nozzle. / Candon, M. J.; Ogawa, H.; Dorrington, G. E.
Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014. Australasian Fluid Mechanics Society, 2014. (Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Candon, MJ, Ogawa, H & Dorrington, GE 2014, Thrust augmentation by after-burning in a scramjet nozzle. in Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014. Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014, Australasian Fluid Mechanics Society, 19th Australasian Fluid Mechanics Conference, AFMC 2014, Melbourne, Australia, 12/8/14.

@inproceedings{e6e847b9d1da468c941d27eeae9d0465,

title = "Thrust augmentation by after-burning in a scramjet nozzle",

abstract = "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.",

author = "Candon, {M. J.} and H. Ogawa and Dorrington, {G. E.}",

year = "2014",

month = jan,

day = "1",

language = "English",

series = "Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014",

publisher = "Australasian Fluid Mechanics Society",

booktitle = "Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014",

note = "19th Australasian Fluid Mechanics Conference, AFMC 2014 ; Conference date: 08-12-2014 Through 11-12-2014",

}

TY - GEN

T1 - Thrust augmentation by after-burning in a scramjet nozzle

AU - Candon, M. J.

AU - Ogawa, H.

AU - Dorrington, G. E.

PY - 2014/1/1

Y1 - 2014/1/1

N2 - 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.

AB - 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.

UR - http://www.scopus.com/inward/record.url?scp=84959152369&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84959152369&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84959152369

T3 - Proceedings of the 19th Australasian Fluid Mechanics Conference, AFMC 2014

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

PB - Australasian Fluid Mechanics Society

T2 - 19th Australasian Fluid Mechanics Conference, AFMC 2014

Y2 - 8 December 2014 through 11 December 2014

ER -

Thrust augmentation by after-burning in a scramjet nozzle

Abstract

Publication series

Conference

All Science Journal Classification (ASJC) codes

Other files and links

Fingerprint

Cite this