Course Description
Discussion of inviscid flow fields over wings in subsonic flow. Vortex lattice methods, lifting surface theories and panel methods developed for wings with attached flow and leading-edge separation. Calculation of aerodynamic characteristics and determination of effects of planform and airfoil shapes.
DE Fee
Engineering Online GRAD
DE Program
MS E
SUM1 10W 2019
Instructors
Classes Start:
May 15, 2019
Classes End:
July 26, 2019
Distance Education:
Yes
Class Type:
Lecture
Credits:
3.00
Delivery Method:
Internet
Restrictions:
Prerequisite: MAE 551 Enrollment for this course is through the Engineering Online Registration System. Go to http://go.ncsu.edu/eol_registration
