Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints

In this study, the optimization of a low-speed wing with functional constraints is discussed. The aerodynamic analysis tool developed by the coupling of the numerical nonlinear lifting-line method to Xfoil is used to obtain lift and drag coefficients of the baseline wing. The outcomes are compared w...

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Veröffentlicht in:	International Journal of Aerospace Engineering Jg. 2019; H. 2019; S. 1 - 14
Hauptverfasser:	Korpe, Durmu Sinan, Kanat, Ozturk Ozdemir
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Cairo, Egypt Hindawi Publishing Corporation 2019 Hindawi John Wiley & Sons, Inc Wiley
Schlagworte:	Aerodynamics Aerospace engineering Aircraft Algorithms Angle of attack Aviation Bending moments Constraints Drag coefficients Engineers Fuel consumption Investigations Low speed Optimization techniques Quadratic programming Reynolds number Shape optimization Shear stress Turbulence models Unmanned aerial vehicles Velocity Weight Wing planforms
ISSN:	1687-5966, 1687-5974
Online-Zugang:	Volltext
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