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Full-Scale Wind-Tunnel Investigation of Wing-Cooling Ducts Effects of Propeller Slipstream, Special Report (1939)
NASA Technical Reports Server (NTRS) · leaf 8
|c sa*-—a : ;—.—•48t'/0* — —— — ■——. ■ —> Figura 1.- Cooling wing with propellere. Figure 5.- Typical variation of duct velocity during take-off. Full-seal® »lnd-tu«a«l duet cooling H tests. Arrangement 7.4-a»-8-6l; nD » 115. <nNASA Technical Reports Server (NTRS)
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