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oaioai:dspace.lib.cranfield.ac.uk:1826/5661

Further tests of a laminar flow swept wing with boundary layer control by suction

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Publication date
1 May 1966
Publisher
Cranfield University, College of Aeronautics

Abstract

Prepared under Ministry of Aviation contract No. KD/18/09/CB63(a

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Cranfield CERES

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Last time updated on 07/02/2012

This paper was published in Cranfield CERES.

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