According to Newton's theory, what happens to the lift to drag value with decreasing angle of attack of a flat plate?

A)
Remains same
B)
Increase monotonically
C)
Decreases parabolically
D)
Becomes zero with maximum angle of attack

Correct Answer :   Increase monotonically


Explanation : The lift/drag ratio for inviscid hypersonic flow over a flat plate is given by :
L/D = cotα
On plotting the curve, as the angle of attack decreases, L/D ratio monotonically increases. Obviously this is a hypothetical condition as skin friction drag is not incorporated in this.