The Course Will Include a Number of Theoretical and Experimental Projects. Theoretical Projects Will Be Concerned With Estimating Stability Derivatives and Acrodynamic Coefficients of a Light Airplane (as Cessna 172) and Consequently, With Estimating Its Performance and Flying Qualities. Experimental Projects Will Be Devoted to In-flight Verification of The Theoretical Estimates.

Faculty: Aerospace Engineering
|Undergraduate Studies

Pre-required courses

(84220 - Flight Mechanics 1 and 84221 - Flight Mechanics 2)


Course with no extra credit

84156 - Advanced Exper.methods in Aerospace Eng. 85222


Semestrial Information