The tests reported herein were made for the purpose of determining the high-speed load distribution on the wing of a 3/16 scale model of a scout-bomber airplane. Comparisons are made between the root bending-moment and section torsional-moment coefficients as obtained experimentally and derived analytically. The results show good correlation for the bending-moment coefficients but considerable disagreement for the torsional-moment coefficients.
High-Speed Load Distribution of the Wing of a 3/16 Scale Model of a Scout-Bomber Airplane with Flaps Deflected
1947
89 pages
Report
Keine Angabe
Englisch