Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at mach number 1.8

Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at mach number 1.8

M. S. Igglesden; L. J. Beecham
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/543
Date: 1961

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