Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

The aerodynamic shape optimization of wings in transonic flow is an inherently challenging problem. In addition to the high computational cost of solving the Reynolds-averaged Navier–Stokes equations, there is a complex interdependence between the cross-sectional shape, wave drag, and viscous effect...

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Veröffentlicht in:	AIAA journal 2016-01, Vol.54 (1), p.113-128
Hauptverfasser:	Kenway, Gaetan K. W, Martins, Joaquim R. R. A
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace engineering Angle of attack Computational fluid dynamics Contours Design analysis Design optimization Drag coefficients Drag reduction Flight conditions Fluid dynamics Maxima Navier-Stokes equations Optimization Performance evaluation Shape optimization Transonic flight Transonic flow Wave drag Wings (aircraft)
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