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Flow visualisation on rolling models using minitufts

Published online by Cambridge University Press:  04 July 2016

C. O. O'Leary
Affiliation:
Royal Aircraft Establishment, Bedford
W. Drew
Affiliation:
Royal Aircraft Establishment, Bedford

Summary

Minitufts are increasingly used for flow visualisation on static wind tunnel models because they can be applied in larger numbers for increased detail and with less interference compared with conventional tufts. This Memorandum describes an extension of their use to continuously rotating models where the heavier conventional tufts are inadequate.

Tests on two combat aircraft models in the 4 m x 2.7 m Low Speed Wind Tunnel are described. Measured variations of rolling moment are explained with the aid of the minituft photographs.

Information

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1987 

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