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Aerodynamic load measurements over a leading-edge slat on a 40 degree sweptback wing at Mach numbers from 0.10 to 0.91

Jones F Cahill, Robert J Nuber

Abstract

Report presenting an investigation of the aerodynamic loads on a leading-edge slat on a 40 degree sweptback wing with NACA 64(sub 1)-112 airfoil sections in the low-turbulence pressure tunnel. Results regarding wing force data, slat force data, and slat pressure distributions are provided.

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Available abstract

Key concepts: Airfoil, Aerodynamics, Wing, Leading edge, Mach number, Trailing edge, Turbulence, Degree (music)