ENGG 140 - Aircraft Performance

Once every three semesters
Examination of performance characteristics of aircraft as a function of propulsion system (turbojet, turbofan, turboprop, piston prop). Optimal conditions for cruise, turning, climb, takeoff and landing. Calculations of best range speed, fuel consumption, and time for maneuvers.

Prerequisites & Notes
ENGG 26, MATH 131. No liberal arts credit.

Credits: 3 s.h.