Experimental study of the low-speed, sectional characteristics of a high-lift airfoil, and comparison of these characteristics with the predictions of the theoretical methods used in the airfoil's design. The 13.1% thick UI-1720 airfoil was found to achieve the predicted maximum lift coefficient of nearly 2.0. No upper-surface flow separation was found below the stall angle of attack of 16 deg; it appeared that stall was due to an abrupt leading-edge flow separation.
Low-speed aerodynamic characteristics of a 13.1-percent-thick, high-lift airfoil
Business Aircraft Meeting ; 1974 ; Wichita, KS
1974-04-01
Conference paper
No indication
English
LOW-SPEED AERODYNAMIC CHARACTERISTICS OF A 13.1-PERCENT-THICK, HIGH-LIFT AIRFOIL*
SAE Technical Papers | 1974
|Low-speed aerodynamic characteristics of a 13.1-percent-thick, high lift airfoil
Tema Archive | 1974
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