Wind tunnel measurements of the lift-dependent drag of thin conically cambered slender delta wings at mach numbers 1.4 and 1.8

Wind tunnel measurements of the lift-dependent drag of thin conically cambered slender delta wings at mach numbers 1.4 and 1.8

M. S. Igglesden
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/532
Date: 1960

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