Design and wind tunnel tests of winglets on a DC-10 wing
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[1] Albert L. Braslow,et al. Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5 , 1958 .
[2] Lawrence C. Montoyu. EFFECT' OF WINGLETS ON A FIRST-GENERATION JET TRANSPORT WING , 1977 .
[3] M. I. Goldhammer. A lifting surface theory for the analysis of nonplanar lifting systems , 1976 .
[4] E. A. Mechtly. The International System of Units: Physical Constants and Conversion Factors. Second Revision , 1973 .
[5] S. G. Flechner,et al. The effect of winglets on the static aerodynamic stability characteristics of a representative second generation jet transport model , 1976 .
[6] S. G. Flechner,et al. A high subsonic speed wind tunnel investigation of winglets on a representative second-generation jet transport wing , 1976 .
[7] Richard T. Whitcomb,et al. A design approach and selected wind tunnel results at high subsonic speeds for wing-tip mounted winglets , 1976 .
[8] C. J. Pirrello,et al. An inventory of aeronautical ground research facilities. Volume 1: Wind tunnels , 1971 .