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Wind-tunnel Investigation at Low Speed of a Wing Swept Back 63 Degrees and Twisted and Cambered for Uniform Load at a Lift Coefficient of 0.5 and with a Thickened Tip Section
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Hubert C Carel
James A Weiberg
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
