Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing

Wind tunnel tests at mach numbers up to 2.80 to determine the effects of changing spanwise volume distribution on a slender, cambered ogee wing

T. A. Cook
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/817
Date: 1965

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