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Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section

D. DUGAN

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Abstract

NACARM A52E01in thesubsonic speedrangeis lessthanone-half maximum airfoil tihick-X ,. nessjandthatutilization of a Wge boattail angleis undesirable..

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NACARM A52E01in thesubsonic speedrangeis lessthanone-half maximum airfoil tihick-X ,. nessjandthatutilization of a Wge boattail angleis undesirable..

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Available abstract

NACARM A52E01in thesubsonic speedrangeis lessthanone-half maximum airfoil tihick-X ,. nessjandthatutilization of a Wge boattail angleis undesirable..

Key concepts: Trailing edge, Wing, Lift-to-drag ratio, Aerodynamics, Drag, Lift (data mining), Angle of attack, Reynolds number

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Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section — Research Paper | ScholarLens