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TECH GENERAL — CH.4
Lift, Drag, and the Angle of Attack
Question 1 of 5
In the lift formula L = Cʟ × ½ρv² × S, the term ½ρv² represents:
A.Static pressure
B.Dynamic pressure
C.Total pressure
D.Wing loading
Question 1 of 5
In the lift formula L = Cʟ × ½ρv² × S, the term ½ρv² represents: