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The effects of aerofoil profile on wing buffet at low speeds

Published online by Cambridge University Press:  04 July 2016

C. A. Lucas  and
D. J. Maull
C. A. Lucas
Affiliation:
The Australian Artificial Intelligence Institute, Carlton, Australia
D. J. Maull
Affiliation:
Cambridge University Engineering Department
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Summary

The unsteady loads on two wings, one exhibiting a trailing edge separation, the other a leading edge separation have been measured. It has been found that there are differences between the two wing loads, one having a large scale viscous-inviscid interaction producing high loads at a low frequency.

Type
Research Article
Information
The Aeronautical Journal , Volume 94 , Issue 933 , March 1990 , pp. 86 - 90
Copyright
Copyright © Royal Aeronautical Society 1990 

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References

1. Mabey, D. G. Beyond the buffet boundary. Aeronaut J, April 1973, 77, (764), pp 201–214.Google Scholar
2. Mabey, D. G. Some Aspects of Aircraft Dynamic Loads due to Flow Separation. Agard R750, 1988.Google Scholar
3. Lucas, C. A. A Study of Wing Buffet. PhD Thesis Cambridge University, 1977.Google Scholar
4. Polentz, P. P., Page, W. A. and Levy, L. L. Jr The unsteady Normal-Force Characteristics of Selected NACA Profiles at High Subsonic Mach Numbers. NACA, RM A55CO2, 1955.Google Scholar