Three-dimensional viscous flow analysis of tip-sail effects on wing performance at low reynolds numbers
dc.contributor.author | Ferley, Dean | |
dc.contributor.examiningcommittee | Chatoorgoon, Vijay (Mechanical and Manufacturing Engineering) Bridges, Greg (Electrical and Computer Engineering) | en_US |
dc.contributor.supervisor | Ormiston, Scott (Mechanical and Manufacturing Engineering) Derksen, Robert (Mechanical and Manufacturing Engineering) | en_US |
dc.date.accessioned | 2015-09-12T19:10:15Z | |
dc.date.available | 2015-09-12T19:10:15Z | |
dc.date.issued | 2015 | |
dc.degree.discipline | Mechanical Engineering | en_US |
dc.degree.level | Master of Science (M.Sc.) | en_US |
dc.description.abstract | Steady, 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.note | October 2015 | en_US |
dc.identifier.uri | http://hdl.handle.net/1993/30772 | |
dc.language.iso | eng | en_US |
dc.rights | open access | en_US |
dc.subject | Tip-Sails | en_US |
dc.subject | Low Reynolds Number | en_US |
dc.subject | CFD | en_US |
dc.subject | Aerodynamics | en_US |
dc.title | Three-dimensional viscous flow analysis of tip-sail effects on wing performance at low reynolds numbers | en_US |
dc.type | master thesis | en_US |