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A study of the three-dimensionalinteraction of wakes and boundarylayers

Published online by Cambridge University Press:  04 July 2016

C. P. Yeung  and
L. C. Squire
C. P. Yeung
Affiliation:
Cambridge University Engineering DepartmentCambridge, UK
L. C. Squire
Affiliation:
Cambridge University Engineering DepartmentCambridge, UK
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Summary

This paper concerns the study of the three-dimensionalinteraction of a slat wake and a wing boundarylayer, as commonly occurs on the suction surface ofa high-lift rnulti-element aerofoil. Theexperimental test case has a realistic slat-wingflow configuration under infinite swept wingconditions. This enables the effect of the crossflow induced by the wing sweep on the slat wake andthe wing boundary layer interaction process to beinvestigated. A triple hot-wire system has been usedto measure the mean velocity and Reynolds stresscomponents in the flow field. The measurements areused to validate a three-dimensional boundary layercode, which has been modified to calculate thisthree-dimensional wake-boundary layer mixingflow.

Information

Type
Research Article
Information
The Aeronautical Journal , Volume 99 , Issue 988 , October 1995 , pp. 343 - 351
Copyright
Copyright © Royal Aeronautical Society 1995 

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