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The lifting two-dimensional aerofoil between slotted walls

Published online by Cambridge University Press:  09 April 2009

A. H. Low
A. H. Low
Affiliation:
School of Mathematics, The University of New South Wales, Kensington, N.S.W.
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Summary

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A mathematical theory is developed which enables the wind-tunnel corrections to the lift and moment forces acting on an aerofoil in subsonic two-dimensional flow to be calculated. The usual “averaged” boundary condition for slotted walls is assumed and the corrections obtained by successive approximation from the open-jet tunnel.

Type
Research Article
Information
Journal of the Australian Mathematical Society , Volume 3 , Issue 2 , May 1963 , pp. 207 - 219
Copyright
Copyright © Australian Mathematical Society 1963

References

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