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Wind-Tunnel Investigation of Control-Surface Characteristics. 20 - Plain and Balance Flaps on an NACA 0009 Rectangular Semi-span Tail Surface

机译:操纵面特性的风洞研究。 20 - 平原和平衡襟翼上的NaCa 0009矩形半翼展尾翼

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摘要

Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balanacing tab was same for sealed plain flap and unsealed overhang flap. Changes in hinge-moment coefficient were diminished by sealing gap. Values measured by three-dimensional flow disagreed with two-dimensional flow values until aspect ratio corrections were made.

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