Transonic Wind-tunnel Investigation of the Low-lift Aerodynamic Characteristics, Including the Effects of Leading Edge Droop and Thickness, of a Thin Trapezoidal Wing in Combination with Basic and Indented Bodies PDF Download

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Transonic Wind-tunnel Investigation of the Low-lift Aerodynamic Characteristics, Including the Effects of Leading Edge Droop and Thickness, of a Thin Trapezoidal Wing in Combination with Basic and Indented Bodies

Transonic Wind-tunnel Investigation of the Low-lift Aerodynamic Characteristics, Including the Effects of Leading Edge Droop and Thickness, of a Thin Trapezoidal Wing in Combination with Basic and Indented Bodies PDF Author: Thomas C. Kelly
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 29

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Book Description
An investigation has been conducted in the Langley 8-foot transonic tunnels to determine the aerodynamic force characteristics at low lift coefficients for a 2-percent-thick trapezoidal wing tested in combination with basic and indented bodies. Effects of wing leading-edge droop and wing thickness are included. Tests extended generally over a Mach number range from 0.80 to 1.43 and an angle-of-attack range from about 0.93 to 0.90.