AERO 633 — Aerodynamics

Equations of motion, vorticity and circulation, conformal mapping and flow round simple bodies. Two-dimensional flow around aerofoils. Flow separation. Flow around finite wings. High and low aspect-ratio wings. Propeller theory and design.

• Credits: 4
• Faculty: Graduate Studies
• Department: Institute for Aerospace Eng.
• Taught by: Jovan Nedic

Sections offered

• Section 001 (Lec), Mon Wed 10:05-11:25 am — 12 seats open
• Section 002 (Lec), Mon Wed 10:05-11:25 am — 5 seats open