Numerical and experimental investigation of aspect ratio effect on aerodynamic performance of NACA 4415 airfoil section at low reynolds number

URN:NBN:SI:doc-XM74MA972025Karadeniz, Ziya HaktanKiral, ZekiÜmütlü Ayaz, Hatice Cansudocuments/doc/X/URN_NBN_SI_doc-XM74MA97_001.pdfdocuments/doc/X/URN_NBN_SI_doc-XM74MA97_001.txt1/271articlestr. 51-572353671712536-3948URN:NBN:SI:doc-XM74MA97engFakulteta za strojništvoStrojniški vestnikInCaerodinamični koeficientiaerodinamični profilaerodynamic coefficientsairfoilaspect ratio effectlow Reynolds numbernizko Reynoldsovo številothree-component balancetri-komponentni merilnik silvetrovnikvitkost krilawind tunnelNumerical and experimental investigation of aspect ratio effect on aerodynamic performance of NACA 4415 airfoil section at low reynolds number