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   Newtonian lift and drag per unit dynamic pressure.
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   Form:
   [cL, cD] = NewtonianLD( reynoldsNo, machNo, alpha, cDParasitic )
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   Inputs
   ------
   alpha       (1,:) Angle of attack (rad)
   machNo      (1,1) Mach Number
   reynoldsNo  (1,1) Reynolds Number (1/length)
   cDParasitic (1,1) Parasitic drag coefficient

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   Outputs
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   cL         (1,:) Lift coefficient
   cD         (1,:) Drag coefficient

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