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Structures

Published online by Cambridge University Press:  28 July 2016

D. J. Farrar
D. J. Farrar*
Affiliation:
Bristol Aircraft Ltd.
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Extract

The main factors determining the shape of a supersonic aeroplane or missile are aerodynamic in origin. However, as always, a compromise with structural considerations must be achieved, zero wing thickness for supersonic aircraft being just as unattainable as infinite aspect ratio for subsonic ones.

This compromise is more far-reaching in the supersonic aircraft because of the much greater importance of aeroelasticity.

In addition, there are entirely new problems which arise from the high structural temperatures attained in supersonic flight.

Information

Type
Supersonic Flight
Information
The Aeronautical Journal , Volume 60 , Issue 551 , November 1956 , pp. 712 - 720
Copyright
Copyright © Royal Aeronautical Society 1956

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References

1.R.A.E. Tech. Note No. Structures 186.Google Scholar
2. Molyneux, W. G. (Unpublished).Google Scholar
3. Broadbent, E. G. (Unpublished).Google Scholar
4. Hartshorn, A. S. (1955). The Temperature of Materials at High Flight Speeds and the Problems Involved. R.A.E. Tech. Note No. Aero 2397. September 1955.Google Scholar
5. Walker, P. B. R.A.E. Report No. Structures 189.Google Scholar
6. Meikle, G. (1953). Summary of the Effect of Heating Some Aluminium Alloys and Alloy Steels at Elevated Temperatures. R.A.E. Tech. Note No. Met. 187. November 1953.Google Scholar
7. Teed, Major P. L. (1953). Titanium–a Survey. Journal of the Royal Aeronautical Society, April 1953.CrossRefGoogle Scholar
8. Sutton, H. (1955). Some Aspects of Modern Aircraft Materials. Journal of the Royal Aeronautical Society, July 1955.CrossRefGoogle Scholar
9. Betteridge, W. (1955). Alloys for Use at High Temperatures. Journal of Institute of Physics, Vol. 6, September 1955.Google Scholar
10. Hoff, N. J. (1951). Structural Problems of Future Aircraft. Proceedings of the Third Anglo-American Aeronautical Conference, September 1951.Google Scholar
11. Parkes, E. W. (1953). Transient Thermal Stresses in Wings. Aircraft Engineering, December 1953.CrossRefGoogle Scholar
12. Keen, E. D. (1953). Integral Construction. Journal of the Royal Aeronautical Society, April 1953.CrossRefGoogle Scholar