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About design and analysis of winglets for military aircraft
The structural design study of the KC-135A winglet installation performance benefits from winglets on the KC-135 aircraft. Dodson, P. C. Brault, .. 35 Preliminary Maximum Bending Stress of Winglet Concepts . basic trapezoid with aspect ratio of 2.33 and taper ratio of 0.338 and a length of 106
Detailed Information
| Author: | Unknown |
|---|---|
| Publication Year: | 2012 |
| Pages: | 216 |
| Language: | English |
| File Size: | 10.53 |
| Format: | |
| Price: | FREE |
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