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A Flight Investigation at Transonic Speeds of the Aerodynamic Characteristics of a Model Having a Thin Unswept Wing of Aspect Ratio 3.1

Maurice D White

Abstract

Report presenting free-falling recoverable-model tests at transonic speeds on a model with a low-aspect-ratio thin unswept wing and a 45 degree swept tail in the chord plane of the wing. Static- and dynamic-stability data and load-distribution data were obtained at a range of angles of attack. Results regarding lift, drag, static longitudinal stability, dynamic longitudinal stability, horizontal-tail effectiveness, loading distribution over the fuselage, and buffet boundary are provided.

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Available abstract

Key concepts: Longitudinal static stability, Transonic, Wing, Wing twist, Fuselage, Wing loading, Aerodynamics, Lift-to-drag ratio