Author:
Bellhouse B. J,Wood C. J.
Abstract
Summary:—Measurements of pressure distribution and skin friction have been made on an 11% thick aerofoil in the presence of a variable base bleed flow. These tests show that the effects of bleed decay rapidly upstream of the base and are measurable only over the rear 40% of the chord. The integrated profile drag values also confirm that wake traverse measurements are subject to error in a strong vortex street.
Publisher
Cambridge University Press (CUP)
Reference4 articles.
1. The Effect of Base Bleed on a Periodic Wake
2. Bellhouse B. J. and Schultz D. L. Determination of Mean Skin Friction, Separation and Transition in Low Speed Flow with a Thin Film Heated Element. To be published.
3. The Measurement of the Drag of Bluff Bodies by the Wake Traverse Method
Cited by
3 articles.
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