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Cessna 172 Simulation Model
Advisor: Prof. Michael Selig
Applied Aerodynamics Group
Department of Aeronautical and Astronautical Engineering
University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Last updated April 10, 2000
This site provides the data needed to model the Cessna 172 small single-engine general aviation aircraft. Currently two versions of this model exist, a linear model using only stability derivatives and a nonlinear model including a lift vs. angle of attack curve to model stall.