Determination of the theoretical pressure distribution for twenty airfoils (1934)
NASA Technical Reports Server (NTRS) · leaf 3
436 KEPOBT NATIONAL ADVISORY COMMITTEE FOE AERONAUTICS … of fig attained by the RA.F. 15 and the N.A.O.A. 0010, 0012, and 2409 airfoils. In particular, the pres- 11. R.A.F.15 sure on the N1.C.A. 0010 reaches — llg for lift coefficient Cx=1.5, whereas the somewhat thicker NA.C1. 0012 reaches — 7q at the same lift coefficient. In practice, the value of…
NASA Technical Reports Server (NTRS)
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