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Wing body interference at supersonic speeds

Kirkby, S.; Robinson, A.

URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/4689

Description:

The increment in lift due to wing-body interference at supersonic speed is calculated approximately for an untapered wing without sweepback.

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COA_Report_No_7_APR_1947.pdf	2.869Mb	application/pdf	View/Open

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CoA. Reports [280]

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