Lecture 3 - Illinois Institute of Technology
Lecture 3 - Illinois Institute of Technology
Lecture 3 - Illinois Institute of Technology
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Next <strong>Lecture</strong>: Finding C M0 and C Mα<br />
The C M0 and C Mα <strong>of</strong> an airplane are determined by adding up the<br />
contributions <strong>of</strong> all factors.<br />
In the next lecture, we will discuss the contributions <strong>of</strong><br />
• Rectangular Wing<br />
• Horizontal Stabilizer<br />
• Canards<br />
M. Peet <strong>Lecture</strong> 3: Nomenclature 36 / 36
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