1955•NASA STI Repository (National Aeronautics and Space Administration)Requires access
Effects of Wing Position and Fuselage Size on the Low-Speed Static Rolling Stability Characteristics of a Delta-Wing Model
Alex Goodman, David Terence Thomas
Open publisher page 5 citations
Abstract
An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of airplane models having a triangular wing and vertical tail surfaces. (author)