A theoretical method of designing cambered slender wings to have low lift-dependent drag is described. The results of subsonic wind tunnel tests on a series of thin cambered delta wings of aspect ratio 2 are presented, and the significant drag reductions achieved are discussed in relation to theoretical predictions for the drag of cambered slender wings. (Author)
Low-Speed Wind-Tunnel Tests on the Lift-Dependent Drag of delta Wings with Conical Camber
1974
39 pages
Report
Keine Angabe
Englisch
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