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Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report (1937)

NASA Technical Reports Server (NTRS) · leaf 11

An illustration from Tests in the Variable-Density Tunnel of Seven Tapered Wings Having N.A.C.A. 230 Mean Lines, Special Report, 1937, leaf 11 — Angle of attack, a (degrees) Lift coefficient CL Figure 4.- Tapered N.A.C.A. 5-10-16 airfoil.

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