Wing-Fuselage Interference, Tail Buffeting, and Air Flow About the Tail of a Low-Wing Monoplane (1935)
NASA Technical Reports Server (NTRS) · leaf 18
r off. McDonnell airplane in original condition. Angle of attack (corrected Angle of attack corrected for tunnel effects. Power off. Air speed approximately for tunnel effect), 3.7° below ctc 58 m.p.h. relative to the lower frequency changes than the record 1. The principal frequency of… … Distance from £, feet I I ./ .a . Scale of vectors: - -■ r. 1+ Deflection 10° 0° in degrees Figure 29—Air flow at tail of McDonnell airplane in original condition, power off. Survey in vertical plane through elevator hinge line. The contours show the ratio of the dynamic pressure behind the…
NASA Technical Reports Server (NTRS)
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