The Effect of Base Bleed on the Flow behind a Two-Dimensional Model with a Blunt Trailing Edge
- 1 August 1967
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 18 (3) , 207-224
- https://doi.org/10.1017/s0001925900004212
Abstract
Summary: The effects of base bleed on the flow about a two-dimensional model with a blunt trailing edge were examined at Reynolds numbers, based on model base height, between 1·3×104 and 4·1×104. The ratio of boundary layer thickness at the trailing edge to half the model base height was approximately 0·4. Measurements were made of base pressure, vortex shedding frequency and the distance to vortex formation. With a sufficiently large bleed quantity the regular vortex street pattern disappeared and the base drag of the section was reduced to about a third of its value without bleed. The base pressure was found to vary linearly with the inverse of the vortex formation distance. Results of a previous splitter plate investigation were found to agree closely with those of the present experiments.Keywords
This publication has 4 references indexed in Scilit:
- Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter platesJournal of Fluid Mechanics, 1965
- The Transonic Flow Past Two-Dimensional AerofoilsJournal of the Royal Aeronautical Society, 1964
- The Effect of Base Bleed on a Periodic WakeJournal of the Royal Aeronautical Society, 1964
- The formation of vortex streetsJournal of Fluid Mechanics, 1962