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How does lift change with airspeed if a constant AOA and altitude are held?(provide specific examples) How does lift change with altitude if a constant
- How does lift change with airspeed if a constant AOA and altitude are held?(provide specific examples)
- How does lift change with altitude if a constant AOA and airspeed are held? (provide specific examples)
- How do the required CL and AOA for your specific aircraft (at a specific weight) changewith changes in airspeed?(provide specific examples)
- What happens if the required CL is larger than CLmaxof your airfoil, and what speed regime is usually associated with that condition
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