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Multidisciplinary Design Optimization of Low-Airframe-Noise Transport Aircraft

Multidisciplinary Design Optimization of Low-Airframe-Noise Transport Aircraft. Leifur Leifsson, William Mason, Joseph Schetz, and Bernard Grossman Virginia Tech and Raphael Haftka, University of Florida. Work sponsored in part by NASA Langley Research Center

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408 views • 24 slides

Configuration Design part 2

Configuration Design part 2. Wing Placement. HIGH WING: PROS. 1. Quick loading and unloading. C-5, C-17 Loading and unloading through nose / tail doors: important to have low floor level.

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360 views • 19 slides

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Te flaps - PowerPoint PPT Presentation

Multidisciplinary Design Optimization of Low-Airframe-Noise Transport Aircraft

Configuration Design part 2