B. Resultant attribute discussions for your selected aircraft Calculated stall speed How does lift change with airspeed ift a constant AOA and altitude are held? (provide specific examples using the correct formula's) How does lift change with altitude ift a constant AOA and airspeed are held? (provide specific examples using the correct formula's) How do the required CL and AOA for your specific aircraft (at a specific weight) change with changes in airspeed? (provide specific examples using the correct formula's) What happens ift the required CL is larger than CL oft your airfoil, and what speed regime is usually associated with that condition