Three-dimensional viscous flow analysis of tip-sail effects on wing performance at low reynolds numbers

dc.contributor.authorFerley, Dean
dc.contributor.examiningcommitteeChatoorgoon, Vijay (Mechanical and Manufacturing Engineering) Bridges, Greg (Electrical and Computer Engineering)en_US
dc.contributor.supervisorOrmiston, Scott (Mechanical and Manufacturing Engineering) Derksen, Robert (Mechanical and Manufacturing Engineering)en_US
dc.date.accessioned2015-09-12T19:10:15Z
dc.date.available2015-09-12T19:10:15Z
dc.date.issued2015
dc.degree.disciplineMechanical Engineeringen_US
dc.degree.levelMaster of Science (M.Sc.)en_US
dc.description.abstractSteady, three-dimensional viscous numerical analysis of airflow over a rectangular NACA 0012 base wing (BW) with a rounded tip and with three NACA 0015 tip-sails (WTS) is performed. The flow physics and aerodynamic forces are studied at Reynolds numbers (Re) of 60,000 and 600,000, angles of attack (α) of 0, 5, 7.5, and 10°, and two sets of tip-sail dihedral angles (leading to trailing tip-sail): 50, 45, and 40° and 60, 45, and 30°. The Shear Stress Transport turbulence and intermittency-transition Reynolds number transitional turbulence models were used. For α > 0°, the WTS produced higher lift coefficients (CL) and drag coefficients (CD) than the BW. At Re = 600,000 and α > 0°, the CL/CD was higher for the WTS than the BW. Good agreement was seen with experimental data at Re = 600,000 for the BW results and the WTS CL but not the WTS CD.en_US
dc.description.noteOctober 2015en_US
dc.identifier.urihttp://hdl.handle.net/1993/30772
dc.language.isoengen_US
dc.rightsopen accessen_US
dc.subjectTip-Sailsen_US
dc.subjectLow Reynolds Numberen_US
dc.subjectCFDen_US
dc.subjectAerodynamicsen_US
dc.titleThree-dimensional viscous flow analysis of tip-sail effects on wing performance at low reynolds numbersen_US
dc.typemaster thesisen_US
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