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Experimental Investigation of Slotted Engine Intakes in the Upper Surface of a Thick Wing
Ronald Anthony Tyler
R. G. Williamson
出版
National Research Council of Canada
, 1968
URL
http://books.google.com.hk/books?id=ikUcNAEACAAJ&hl=&source=gbs_api
註釋
The effects of flow rates appropriate to engine requirements through slotted intakes in the rear upper surface of a thick wing were investigated. The basic test configuration incorporated a 31.5 percent thick aerofoil of 3-ft chord and 4-ft span. The aerofoil was equipped with a wide (5 percent chord), full span intake slot, located at 65 percent chord, and operated at values of suction coefficient up to 0.20. Measured results relating to aerofoil force characteristics and intake losses are presented and discussed. (Author).
