Analysis of spinning in a monoplane wing by the induction method as compared with the strip method (1934)
NASA Technical Reports Server (NTRS) · leaf 40
T.l.C.X. Technical Monorandun So. 747 riga. 4a,4"b. 0.2 0.26 0.3 U)z 0.1 0.02 0.04 0.06 Coefficients ro^ and mz tfigure 4a.- lionents due to rotation about axLe of notion, co £a 0 for Aq b 0.6 Coefficients vt» • and n … ligore 4b.- Moments due to rotations about axis of notionui g ■ 0 for Aq = 0.6
NASA Technical Reports Server (NTRS)
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