1957•Unpublished venueRequires access

Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03

F E West, Charles F Whitcomb, James W Schmeer

Abstract

Report discussing an investigation of a 45 degree swept-back-wing-body combination with flap spoiler ailerons, deflector ailerons, and a spoiler-slot-deflector aileron. The pressures were measured from Mach numbers 0.60 to 1.03 and at various angles of attack.

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Key concepts: Aileron, Mach number, Wing, Aerodynamics, Angle of attack, Aerospace engineering, Engineering