Physical insight into scramjet inlet behaviour via multi-objective design optimisation

H. Ogawa, R. R. Boyce

Research output: Chapter in Book/Report/Conference proceedingConference contribution

2 Citations (Scopus)

Abstract

Scramjet propulsion is a promising technology for reliable and economical access to space and high-speed atmospheric transport. The inlet plays a key role in determining the performance of scramjets, in particular for the axisymmetric class of scramjet engines that are currently explored due to their advantages in numerous aspects. In the present study a multi-objective design optimisation (MDO) has been conducted with respect to four major inlet design criteria: compression efficiency, drag, adverse pressure gradient, and exit temperature. The former three criteria are used as the objective functions and the last as the constraint function to evaluate the inlet flowfields in the state-of-the-art coupled CFD / MDO approach. The influential parameters and key physics have been identified by scrutinising the flowfields that have been obtained as an outcome of the optimisation.

Original languageEnglish
Title of host publication27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
Pages2790-2800
Number of pages11
Publication statusPublished - Dec 1 2010
Event27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 - Nice, France
Duration: Sep 19 2010Sep 24 2010

Publication series

Name27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
Volume4

Other

Other27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010
CountryFrance
CityNice
Period9/19/109/24/10

Fingerprint

Pressure gradient
Propulsion
Drag
Computational fluid dynamics
Physics
Engines
Temperature
Design optimization

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Materials Science(all)

Cite this

Ogawa, H., & Boyce, R. R. (2010). Physical insight into scramjet inlet behaviour via multi-objective design optimisation. In 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010 (pp. 2790-2800). (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010; Vol. 4).

Physical insight into scramjet inlet behaviour via multi-objective design optimisation. / Ogawa, H.; Boyce, R. R.

27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. p. 2790-2800 (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010; Vol. 4).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Ogawa, H & Boyce, RR 2010, Physical insight into scramjet inlet behaviour via multi-objective design optimisation. in 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010, vol. 4, pp. 2790-2800, 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010, Nice, France, 9/19/10.
Ogawa H, Boyce RR. Physical insight into scramjet inlet behaviour via multi-objective design optimisation. In 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. p. 2790-2800. (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010).
Ogawa, H. ; Boyce, R. R. / Physical insight into scramjet inlet behaviour via multi-objective design optimisation. 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010. 2010. pp. 2790-2800 (27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010).
@inproceedings{42d1ddaea38e47b0903e1befb296b437,
title = "Physical insight into scramjet inlet behaviour via multi-objective design optimisation",
abstract = "Scramjet propulsion is a promising technology for reliable and economical access to space and high-speed atmospheric transport. The inlet plays a key role in determining the performance of scramjets, in particular for the axisymmetric class of scramjet engines that are currently explored due to their advantages in numerous aspects. In the present study a multi-objective design optimisation (MDO) has been conducted with respect to four major inlet design criteria: compression efficiency, drag, adverse pressure gradient, and exit temperature. The former three criteria are used as the objective functions and the last as the constraint function to evaluate the inlet flowfields in the state-of-the-art coupled CFD / MDO approach. The influential parameters and key physics have been identified by scrutinising the flowfields that have been obtained as an outcome of the optimisation.",
author = "H. Ogawa and Boyce, {R. R.}",
year = "2010",
month = "12",
day = "1",
language = "English",
isbn = "9781617820496",
series = "27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010",
pages = "2790--2800",
booktitle = "27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010",

}

TY - GEN

T1 - Physical insight into scramjet inlet behaviour via multi-objective design optimisation

AU - Ogawa, H.

AU - Boyce, R. R.

PY - 2010/12/1

Y1 - 2010/12/1

N2 - Scramjet propulsion is a promising technology for reliable and economical access to space and high-speed atmospheric transport. The inlet plays a key role in determining the performance of scramjets, in particular for the axisymmetric class of scramjet engines that are currently explored due to their advantages in numerous aspects. In the present study a multi-objective design optimisation (MDO) has been conducted with respect to four major inlet design criteria: compression efficiency, drag, adverse pressure gradient, and exit temperature. The former three criteria are used as the objective functions and the last as the constraint function to evaluate the inlet flowfields in the state-of-the-art coupled CFD / MDO approach. The influential parameters and key physics have been identified by scrutinising the flowfields that have been obtained as an outcome of the optimisation.

AB - Scramjet propulsion is a promising technology for reliable and economical access to space and high-speed atmospheric transport. The inlet plays a key role in determining the performance of scramjets, in particular for the axisymmetric class of scramjet engines that are currently explored due to their advantages in numerous aspects. In the present study a multi-objective design optimisation (MDO) has been conducted with respect to four major inlet design criteria: compression efficiency, drag, adverse pressure gradient, and exit temperature. The former three criteria are used as the objective functions and the last as the constraint function to evaluate the inlet flowfields in the state-of-the-art coupled CFD / MDO approach. The influential parameters and key physics have been identified by scrutinising the flowfields that have been obtained as an outcome of the optimisation.

UR - http://www.scopus.com/inward/record.url?scp=84878487672&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84878487672&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84878487672

SN - 9781617820496

T3 - 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010

SP - 2790

EP - 2800

BT - 27th Congress of the International Council of the Aeronautical Sciences 2010, ICAS 2010

ER -