1941•Unpublished venueRequires access

Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics III : Symmetrically Tapered Wing at Various Positions on Circular Fuselage with and Without a Vertical Tail

Isadore G Recant, Arthur R Wallace

Abstract

Report presenting testing of model combinations of an NACA 23012 tapered wing and a circular fuselage to determine the effect of longitudinal wing position on the change in lateral stability due to interference. Results regarding wing-fuselage interference and effect of wing-fuselage interference on vertical tail are provided.

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Available abstract

Key concepts: Fuselage, Wing, Interference (communication), Longitudinal static stability, Structural engineering, Wind tunnel, Engineering, Aerospace engineering