Numerical analysis and optimization of a winglet sweep angle and winglet tip chord for improvement of aircraft flight performance
In the present research, an investigation of the influence of winglet sweep angle and winglet tip chord of the aircraft wing on the aerodynamics properties and how to make it better has been carried out, assuming Cant angle 60, winglet height = 3.5 m, Toe angle = -5, and Twist angle = +5. Sweep angl...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Polskie Towarzystwo Diagnostyki Technicznej
2022-06-01
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| Series: | Diagnostyka |
| Subjects: | |
| Online Access: | http://www.diagnostyka.net.pl/Numerical-analysis-and-optimization-of-a-winglet-sweep-angle-and-winglet-tip-chord,150479,0,2.html |