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Low-speed Investigation of the Effects of Nacelles on the Longitudinal Aerodynamic Characteristics of a 60 Degree Sweptback Delta-wing - Fuselage Combination with NACA 65A003 Airfoil Sections

W. I. Scallion

Abstract

Report presenting an investigation in the full-scale tunnel to determine the effects of symmetrically located wing nacelles on the low-speed aerodynamic characteristics of a 60 degree sweptback delta-wing-fuselage combination. The testing occurred with three spanwise nacelle locations with three chordwise positions at each spanwise station.

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Available abstract

Key concepts: Nacelle, Fuselage, Airfoil, Aerodynamics, Wing, Delta wing, Structural engineering, Aerospace engineering