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Some Aspects of Flight Research

Published online by Cambridge University Press:  28 July 2016

Handel Davies
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Extract

Aeronautics has advanced a long way since that December day in 1903 when Wilbur and Orville Wright successfully completed the first flight test ever to be made on a powered aircraft. Since then much has been learnt about the science of aeronautics and great developments have taken place in the methods and techniques of aeronautical research. Wind tunnels have been built capable of testing models at very high speeds and at high Reynolds numbers, and many other powerful research techniques have been developed to assist in the design of aircraft. The behaviour of the aircraft itself in flight remains the final test, however, and there are still many problems which can be investigated adequately only in flight with a piloted aircraft.

In this lecture it is proposed to illustrate the contribution which flight research can make towards the advancement of knowledge of aeronautics by discussing some of the more important aspects of this work.

Type
Research Article
Information
The Aeronautical Journal , Volume 55 , Issue 486 , June 1951 , pp. 325 - 361
Copyright
Copyright © Royal Aeronautical Society 1951

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References

1. Richards, E. J. (1950). A Review of Aerodynamic Cleanness. Journal of the Royal Aeronautical Society, March 1950.Google Scholar
2. Fage, A. (1943). The Smallest Size of a Spanwise Surface Corrugation which Affects Boundary Layer Transition on an Aerofoil. R. & M. No. 2120.Google Scholar
3. Smith, F. and Higton, D. J. (1950). Flight Tests on King Cobra FZ 440 to investigate the practical requirement for the achievement of low profile drag coefficients on a “ low drag aerofoil.” R. & M. No. 2375.Google Scholar
4. Plascott, R. H., Higton, D. J. and Smith, F. Flight tests on Hurricane II Z 3687 fitted with special wing of low drag design. R. & M. 2546.Google Scholar
5. Goldstein, S. (1948). Low-drag and Suction Aerofoils. Journal of the Aeronautical Sciences, April 1948.Google Scholar
6. Davies, H. (1948). Flight Research at High Subsonic Speeds. Journal of the Royal Aeronautical Society, May 1948.Google Scholar
7. Higton, D. J., Plascott, R. H. and Clarke, , —. —. Measurement of Overall Drag of an Aircraft (to be published as an R. & M.). R.A.E. Aero Reports Nos. 2241 and 2309.Google Scholar
8. Hills, R. (1951). Use of Wind Tunnel Model Data in Aerodynamic Design. Journal of the Royal Aeronautical Society, January 1951.Google Scholar
9. White, R. J. (1950), Investigation of Lateral Dynamic Stability in the XB-47 Airplane. Journal of the Aeronautical Sciences, March 1950.Google Scholar
10. Kauffman, W. M., Liddell, C. J. Jr., Smith, A. and Van Dyke, R. D. Jr. (1949). An Apparatus for Varying Effective Dihedral in Flight with Application to a Study of Tolerable Dihedral on a Conventional Fighter Airplane. N.A.C.A. Report 948, August 1949.Google Scholar
11. Morgan, M. B. (1947). Control in Low Speed Flight. Anglo-American Conference, London, 1947.Google Scholar
12. Morgan, M. B. and Thomas, H. H. B. M. (1945). Control Surface Design. Journal of The Royal Aeronautical Society, August 1945.Google Scholar
13. Lyons, D. J. (1949). Present Thoughts on the Use of Powered Flying Controls in Aircraft. Journal of the Royal Aeronautical Society, March 1949.CrossRefGoogle Scholar
14. Lyons, D. J. (1948). Some Problems of the Stability and Control of Large Aircraft. Journal of the Royal Aeronautical Society, November 1948.CrossRefGoogle Scholar
15. Rogallo, F. M., Lowry, J. G. and Fischel, J. (1950). Lateral Control Devices Suitable for Use with Full-span Flaps. Journal of the Aeronautical Sciences, October 1950.Google Scholar
16. Young, A. D. Lateral Control with High Lift Devices (with Appendix by R. R. Duddy). R. & M. (to be published).Google Scholar
17. Ashkenas, I. L. (1946). Development of Lateral Control System for Use with Large Span Flaps. N.A.C.A. T.N. 1015, January 1946.Google Scholar
18. Gilruth, R. R. (1947). Résumé and Analysis of N.A.C.A. Wing Flow Tests. Anglo-American Conference, London, 1947.Google Scholar
19. Northrop, J. K. (1947). The Development of All-wing Aircraft, Journal of the Royal Aeronautical Society, June 1947.CrossRefGoogle Scholar
20. Gray, W. E. (1950). A Chemical Method of Indicating Transition in the Boundary Layer, and some Flight Results on a Low Drag Wing. R. & M. To be published.Google Scholar
21. Lamplough, F. E. (1951). Shock-Wave Shadow Photography in Tunnel and in Flight. Aircraft Engineering, April 1951.Google Scholar