The 7 by 10 Foot Wind Tunnel of the National Advisory Committee for Aeronautics (1933)
NASA Technical Reports Server (NTRS) · leaf 8
essure wing-rotating device (fig. 5) on the framework in place and air stream angularity surveys were made at the of the force-test model support. The mountings of model location, 2 feet 10 inches downstream from the both the rotating device and the force-test spindle are entrance cone. Seventy… … Figure 5.—Rotation-test model Bupporl the ratio of the kinetic energy per second of the air flowing through the jet to the electrical energy input The rotation-test model support (fig. 5) consists of a per second to the motor. The energy ratio of the horizontal spindle supported in a housing A on…
NASA Technical Reports Server (NTRS)
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