Flight Test Engineering

Catalog description

Credits 3. 2 Lecture Hours. 3 Lab Hours. Application of performance and stability and control theory to flight test measurements; standard atmosphere and airspeed equations for pilot-static system calibrations; flight test methods for evaluating performance, stability and control, and stall-spin characteristics; laboratory practice in planning and conducting small flight test project. Prerequisite: Grade of C or better in AERO 321 .