# Cessna 172 Simulation Model

Graduate Research done by Jeff Scott
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.

## Go to

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- Linear Model
- Nonlinear Model
- References

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