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Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel (1931)

NASA Technical Reports Server (NTRS) · leaf 10

An illustration from Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel, 1931, leaf 10 — 9 AIRFOIL PRESSURE DISTRIBUTION INVESTIGATION … -8° 0° 8° 16° 2*° 32° a -B O .2 .4 CM Figure 6.—Pressure distribution on N. A. C. A. 84 airfoil

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$An illustration from Opticks, or, A treatise of the reflexions, refractions, inflexions and colours of light ; Also two treatises of the species and magnitude of curvilinear figures (1704)$