Hypersonic Aerothermodynamics - AAE51900
Aerodynamics of satellites and planetary re-entry. Continuum hypersonic flow. Inviscid and viscous effects, boundary layers, and heat transfer. Shock and boundary-layer interactions. Equilibrium flow of high-temperature reacting gases. Nonequilibrium effects. Kinetic theory and rarefied flows. Direct simulation Monte Carlo techniques.
Credit Hours: 3
Instructor(s): Steven Schneider
Phone: (765) 494-3343
Email: steves@purdue.edu
Office: Room 13C AERO (Hangar 3)
Applied / Theory: 50 / 50
Web Address: https://engineering.purdue.edu/~aae519/