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MECH 581 101 (Lecture)

Low Speed Aerodynamics

Circulation, vorticity and Kelvin's Theorem. Potential flow theory and the Kutta-Joukowski Law 2D Vortex Panel. Method. Laminar and turbulent boundary layer computations. Lifting line theory. Vortex Lattice Method. High lift devices. Total airplane drag. Credit cannot be obtained for both MECH 581 and MECH 481.

This course is not eligible for Credit/D/Fail grading.

Credits: 3

Location: Vancouver

Term 1 (Sep 03, 2019 to Nov 29, 2019)

Withdrawal Dates
Last day to withdraw without a W standing : September 17, 2019
Last day to withdraw with a W standing
(course cannot be dropped after this date) :
October 11, 2019

TermDay Start TimeEnd TimeBuildingRoom
1 Mon Wed13:0014:00Civil and Mechanical Engineering1215

Seat Summary
Total Seats Remaining:1
Currently Registered:4
General Seats Remaining:1
Restricted Seats Remaining*:0
-  Select one Laboratory from sections L1A

Book Summary :
Information for the books required for this section is not available.