Aerospace Propulsion

Undergraduate

Application of gas dynamics and thermodynamics to aerospace engines. Analysis of engine cycles. Theory and design of propellers; turboprop engine analysis, Internal combustion and gas turbine engines. Component design for compressors, combustors, afterburners, exhaust nozzles. (Pre-requisites: MECH- 3217, MECH-3220, MECH-3670, and semester 7 or higher standing.)