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- W566752009 abstract "Aasc = (0.25) ( 1 . 0 7 8 C L ) = 0.269 CL (3) A similar example using the unit vortex approach (page 22 of reference 4) yields a value of 0 . 2 5 4 C L . The difference of 0.015° (at CL — 1.0) is not surprising in view of the uncertainties of the extrapolation and the fact that reference 4 uses an average value rather than that at the centerline. Better agreement would reasonably be expected for a floor mounted model, since the tunnel shape would then be more reasonable. (4) At M = 0.85, lt/B(l M ) / 2 = 0.0307/[1 (0.85)] = 0.0583 and r = 0.475. Aasc then equals (0.475) (1.078CL) = 0MSCL." @default.
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- W566752009 date "1954-04-01" @default.
- W566752009 modified "2023-09-27" @default.
- W566752009 title "Wind-Tunnel Model Position for Transonic Testing" @default.
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- W566752009 doi "https://doi.org/10.2514/8.2995" @default.
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