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MECH 481 101 (Lecture)

Aerodynamics of Aircraft I

Analysis of airfoils and wings. Potential flow, thin airfoil theory, lifting line analysis of wings. Predicting viscous drag. Numerical methods for analysis and design of airfoils and wings. Use of wind tunnels for experimental study of aerodynamics.

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
Note: this section is restricted

Seat Summary
Total Seats Remaining:12
Currently Registered:25
General Seats Remaining:0
Restricted Seats Remaining*:12
    *These seats are reserved for students who meet one of the following sets of restrictions:
  1. in one of these programs: BASC in year: >=3
-  Select one Laboratory from sections L1A

Book Summary :
Title Reqd/Opt/Rel Author ISB
Introduction to Theoretical and Computational Aerodynamics Required MORAN 9780486428796