Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptback, sweptforward, and yawed wings. The tests covered changes in aspect ratio, taper ratio, and tip shape. Some data were obtained with high-lift devices on sweptback wings and with ailerons on sweptforward wings. The data have been briefly analyzed and some comparisons have been made with the available theory.
Wind-tunnel Tests at Low Speed of Swept and Yawed Wings Having Various Plan Forms
01.12.1951
Sonstige
Keine Angabe
Englisch
Calculation of tunnel-induced upwash velocities for swept and yawed wings
Engineering Index Backfile | 1948
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