Hostname: page-component-cb9f654ff-plnhv Total loading time: 0.001 Render date: 2025-08-24T11:09:08.005Z Has data issue: false hasContentIssue false

Aerodynamic technology — the role ofaerodynamic technology in the design and developmentof modern combat aircraft

Published online by Cambridge University Press:  04 July 2016

T. McMichael
Affiliation:
British Aerospace, Military Aircraft Division, UK
K. McKay
Affiliation:
British Aerospace, Military Aircraft Division, UK
M.J. Walker
Affiliation:
British Aerospace, Military Aircraft Division, UK
C. Fielding
Affiliation:
British Aerospace, Military Aircraft Division, UK
G. Lockley
Affiliation:
British Aerospace, Military Aircraft Division, UK
P. Curtis
Affiliation:
British Aerospace, Military Aircraft Division, UK
B. Probert
Affiliation:
British Aerospace, Military Aircraft Division, UK
C. S. Lee
Affiliation:
British Aerospace, Military Aircraft Division, UK
G. Moretti
Affiliation:
British Aerospace, Military Aircraft Division, UK

Abstract

This paper examines the changing role aerodynamictechnology plays in the design and development ofmodern combat aircraft. It reviews several aspectsof aerodynamics which contribute to aircraftperformance and handling characteristics. Itconsiders the importance of a range of technologies,the contribution each makes to the final integratedsolution and comments on the compromises necessarythrough the design cycle to optimise the overallweapon system, sometimes to the cost of one of thecomponent technologies. The technologies discussedare in no way exhaustive but attempt to encapsulatethe breadth of the subject, to illustrate itsdiversity and to point the way for the futuredevelopment if aerodynamic technology is to continueto make an important contribution to the design ofcombat aircraft.

Each of the component technologies are discussed interms of the contribution it makes, the tools andtechniques used to predict, analyse and interpretthe technology contribution, and the requirementsfor the direction of the development of thetechnology for the future.

Before considering the technologies themselves it isimportant to understand the environment in whichthey will be used, which increasingly conditions themanner in which they are employed and suggests thedirection for their development.

This paper begins, therefore, by briefly reviewing thechanges to the environment in which the fighterpilot operates and the manner by which hisrequirements, and therefore the specification of theaircraft, are defined before going on to look at theoverall contribution each technology makes in thedesign process.

Information

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1996 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

Article purchase

Temporarily unavailable

References

1.AGARD Flight Mechanics Panel WG-19 AR-314 Operational Agility.Google Scholar
2. Nelson, J.R. and Smith, T.D. Improved combat performance using relaxed static stability and a spin prevention system (FBW Jaguar), AGARD conference proceedings No 409, 1986.Google Scholar
3. McCuich, A. and Caldwell, B. Development of flight experience of the control laws and the aeroelastic solution in the Experimental Aircraft Programme, In: Advances in Flight Control, Taylor and Francis, 1996.Google Scholar
4. Gibson, J.C. The Definition, Understanding and Design of Aircraft Handling Qualities, Delft University of Technology report LR-756, 1995.Google Scholar
5. Ramsay, R.B. AGARD Conference Proceeding No 556 Flight flutter testing of combat aircraft.Google Scholar
6. Shanks, G., Gale, S., Fielding, C. and Griffith, D. Flight control and handling research with the VAAC Harrier aircraft. Advances in Flight Control, Taylor and Francis, 1996.Google Scholar