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Effect of the Angular Position of the Section of a Ring Cowling on the High Speed of an XF7C-1 Airplane (1930)
NASA Technical Reports Server (NTRS) · leaf 16
Fig.1,9. N.A.C.A. Technical Not© No.355 Fig.9 View of cowling set at -8.8 degrees on fuselage No.3NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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