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Share Pages by iraq0917 is a document available to read on EtoBox.
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This technical report details the design and analysis of winglets for military aircraft, specifically the KC-135 and C-141 models. The analysis indicated significant reductions in induced drag and improvements in performance metrics, with a 14% drag reduction for the KC-135 and an estimated weight increase of 592 lbs for the winglet installation. The report includes various studies on winglet parameters and concludes with the final design and analysis for the KC-135 aircraft.
- Author
- iraq0917
- Language
- EN