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Investigation in the 7-By-10 Foot Wind Tunnel of Ducts for Cooling Radiators Within an Airplane Wing, Special Report (1938)

NASA Technical Reports Server (NTRS) · leaf 34

An illustration from Investigation in the 7-By-10 Foot Wind Tunnel of Ducts for Cooling Radiators Within an Airplane Wing, Special Report, 1938, leaf 34 — .2 A .6 .8 1.0 1.2 1.4 Section lift coefficient, ct Section lift coefficient, c, t-> Figure 13a Figure 13b sb

NASA Technical Reports Server (NTRS)

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