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Thin Airfoil Theory - Virginia Tech
3 Thin Airfoil Theory - Simplifications Bernoulli: Kutta Condition: u=V cos +u' v=V sin +v' x c V(c,0 V(c,0 y Assumptions: 1. Airfoil is thin << c 2. Angles/slopes are small e.g.
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Chapter 4 Attitude Determination - Virginia Tech
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General guidelines for technical writing - Virginia Tech
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