53 lines
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1.3 KiB
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53 lines
No EOL
1.3 KiB
HTML
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<title>Cessna 172 Simulation Model</title>
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<BODY
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bgcolor="FFFFFF" text="000000" link="0800FF"
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vlink="FF0000" alink="FF0FF8">
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<font face="arial,helvetica">
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<center><h1><b><i>
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Cessna 172 Simulation Model
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</i></b></h1></center>
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<b><i>Graduate Research done by <a href="http://fly.to/jeffscott/">Jeff Scott</a><br>
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Advisor: <a href="http://www.uiuc.edu/ph/www/m-selig">Prof. Michael Selig</a><br>
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Applied Aerodynamics Group<br>
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Department of Aeronautical and Astronautical Engineering<br>
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University of Illinois at Urbana-Champaign, Urbana, Illinois 61801<p>
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Last updated April 10, 2000</i></b>
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<p>
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This site provides the data needed to model the Cessna 172 small
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single-engine general aviation aircraft. Currently two versions of
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this model exist, a linear model using only stability derivatives
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and a nonlinear model including a lift vs. angle of attack curve to
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model stall.
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<p>
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<h2>Go to</h2>
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<ul><h3>
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<li><a href="linear.html">Linear Model</a></li>
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<li><a href="nonlinear.html">Nonlinear Model</a></li>
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<li><a href="refs.html">References</a></li>
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</h3></ul>
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<p>
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<hr>
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<p>
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<h3><b><center>
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<a href="../index.html">Back to Aircraft Models</a> *
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<a href="http://amber.aae.uiuc.edu/~jscott/sis/">Go to SIS Flight Sim page</a>
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</h3></b></center>
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