Hostname: page-component-78c5997874-v9fdk Total loading time: 0 Render date: 2024-11-17T21:31:41.620Z Has data issue: false hasContentIssue false

Structural Problems of Advanced Aircraft

Published online by Cambridge University Press:  28 July 2016

Extract

In assessing the true extent of technical development of any kind the mind naturally seeks a standard for comparison. When considering structural development the standard chosen could well be that associated with the end of the Second World War. In preparing this paper, therefore, it appeared profitable, and certainly it has been extremely interesting for the author, to review the structure of some of the aircraft then in quantity production.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1952

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. Hoff, N. J. (1951). Structural Problems of Future Aircraft, Third Anglo-American Aeronautical Conference, Brighton. The Royal Aeronautical Society, 1952.Google Scholar
2. Peery, D. (1950). Aircraft Structures, McGraw-Hill, New York, 1950.Google Scholar
3. Teed, P. L. (1949). Application of Materials, Second Anglo-American Aeronautical Conference, New York, Institute of the Aeronautical Sciences, 1949.Google Scholar
4. Collar, A. R. (1946). The Expanding Domain of Aeroelasticity, Journal of the Royal Aeronautical Society, August 1946.CrossRefGoogle Scholar
5. Collar, A. R. (1947). Aeroelastic Problems at High Speed, Journal of the Royal Aeronautical Society, January 1947.CrossRefGoogle Scholar
6. Collar, A. R., Broadbent, E. G. and Puttick, E. B. (1946). An Elaboration of the Criterion for Wing Torsional Stiffness. R. & M. 2154, January 1946.Google Scholar
7. Williams, D. (1947). Some Novel Structural Properties of Stressed Skin Wings. First Anglo-American Aeronautical Conference, London. The Royal Aeronautical Society, 1948.Google Scholar
8. Hill, G. T. R. (1951). Advances in Aircraft Structural Design. Third Anglo-American Aeronautical Conference, Brighton. The Royal Aeronautical Society, 1952.Google Scholar