The Variable Density Wind Tunnel of the National Advisory Committee for Aeronautics (1926)
NASA Technical Reports Server (NTRS) · leaf 17
16 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Fig. 14.—Variable density wind tunnel dynamic pressure survey. Observations taken at 161 different points. Pressures are in per cent of arbitrary reference point. Plane of survey —49.5" in rear of honeycomb. Rectangle at center indicates approximate position of airfoil 0 10 20 30 40 50 60 Inches…
NASA Technical Reports Server (NTRS)
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