Hostname: page-component-78c5997874-fbnjt Total loading time: 0 Render date: 2024-11-17T19:36:49.509Z Has data issue: false hasContentIssue false
  • English
  • Français

Computer aided aircraft project design

Published online by Cambridge University Press:  04 July 2016

H. P. Y. Hitch
H. P. Y. Hitch*
Affiliation:
British Aircraft Corporation, Commercial Aircraft Division
Get access Rights & Permissions [Opens in a new window]

Extract

The computer can be used in many ways to assist in the project and design stages of aircraft development. As would be expected it was used first to assist in the more unwieldy calculations of the design stage. Massive calculation sequences which previously involved much tedious labour, or were effectively beyond the capacity of a design office to perform, suddenly became a few hours work for one or two technicians. Project analysis, being concerned with an earlier stage of development where calculations are simpler and more approximate, tended to remain largely unaffected. However, it became clear that the very simplicity of the preliminary project calculations would, at least in principle, allow the entire project analysis phase to be computerised, so allowing many parametric variations to be done in a short time with minimum effort. The natural follow-on to this was the optimising project analysis program of which examples now exist. With such programs one is able to predict an optimum configuration to meet a given requirement, given only the basic data to define the scope of the calculation.

Type
Research Article
Information
The Aeronautical Journal , Volume 81 , Issue 794 , February 1977 , pp. 51 - 62
Copyright
Copyright © Royal Aeronautical Society 1977 

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.)

References

1. Peckham, D. H. Multivariate analysis applied to aircraft optimisation—a first progress report. RAE Tech Memo Aero 1352. September 1971.Google Scholar
2. Piggott, B. A. M. and Taylor, B. E. Application of numerical optimisation techniques to the preliminary design of a transport aircraft. RAE Tech Report 71074, 1971.Google Scholar
3. Kirkpatrick, D. L. I. and Collingbourne, Joan. Multivariate analysis applied to aircraft optimisation—a second progress report. RAE Tech Memo Aero 1552, November 1973.Google Scholar
4. Straub, Jnr., William, L. Managerial implications of computerised aircraft design synthesis. Journal of Aircraft, March 1974.Google Scholar
5. Wallace, R. E. A computerised system for the preliminary design of commercial airplanes. AIAA Paper 72-793, 1972.Google Scholar
6. Fulton, R. E. and Landrum, E. J. An integrated computer system for preliminary design of advanced aircraft. AIAA Paper 72-796, 1972.Google Scholar
7. Peyton, R. S. An aerodynamics model applicable to the synthesis of conventional fixed wing aircraft. Paper 908, Society of Aeronautical Weight Engineers, May 1972.Google Scholar
8. Herbst, W. B. and Ross, H. Application of computer-aided design programs for the technical management of complex fighter development projects. AIAA Paper 70-364, 1970.Google Scholar
9. Ladner, F. K. and Roch, A. J. A summary of the design synthesis process. Paper 907, Society of Aeronautical Weight Engineers, May 1972.Google Scholar
10. Baals, D. D., Robins, A. W. and Harris, R. V. Jnr. Aerodynamic design integration of supersonic aircraft. AIAA Paper 68-1018, 1968.Google Scholar
11. McNeal, R. H. The NASTRAN Theoretical Manual. NASA SP-221. September 1970.Google Scholar
12. Crookes, W. A., Cooper, P. J. and Webb, E. CAPS: A computer-based aid to aircraft project studies. Computer Aided Design. April 1974.Google Scholar
13. Ardema, M. R. and Williams, L. J. Automated Synthesis of Transonic Transports. AIAA Paper 72-794, 1972.Google Scholar
14. Galloway, T. L. and Waters, M. H. Computer-aided parametric analysis for general aviation aircraft. SAE Paper 730332, 1973.Google Scholar
15. Kirkpatrick, D. L. I. and Peckham, D. H. Multivariate analysis applied to aircraft optimisation—some effects of research advances on the design of future transport aircraft. RAE Tech Memo Aero 1448, September 1972.Google Scholar
16. Edwards, J. B., Kirkpatrick, D. L. I. and Edwards, J. B. W. A forecast of CTOL transport aircraft developments including the effect of a fuel price increase. RAE Tech Memo Aero 1529, July 1973.Google Scholar
17. Bishop, A. W. Optimisation in aircraft design—the whole aircraft. RAeS Symposium, November 1972.Google Scholar
18. Kondo, Jiro. Computer-aided design of Civil Transport Plane. Transactions of the Japan Society for Aeronautical & Space Sciences, 1970.Google Scholar
19. Bishop, A. W. and Page, A. N. An approach to Design Integration. AGARD-CP-147, Vol 1 (Aircraft Design Integration and Optimisation), June 1974.Google Scholar