1950•Unpublished venueRequires access

Low-speed investigation of leading-edge and trailing-edge flaps on a 47.5 degree sweptback wing of aspect ratio 3.4 at a Reynolds number of 4.4 x 10(exp 6)

Jerome Pasamanick, Thomas B Sellers

Abstract

Report presenting an investigation in the full-scale tunnel of the low-speed longitudinal characteristics of a 47.5 degree sweptback wing-fuselage combination with various extensible leading-edge-flap and plain trailing-edge-flap arrangements. Results regarding the basic longitudinal characteristics, extensible leading-edge flaps, plain trailing-edge flaps, and flap combinations are provided.

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Available abstract

Key concepts: Trailing edge, Leading edge, Reynolds number, Enhanced Data Rates for GSM Evolution, Fuselage, Wing, Materials science, Structural engineering