Enlist the computer methods used which benefitted the airfoil performance along with wind- tunnel testing.

A)
Panel method
B)
Hit – and – trial methods
C)
Advanced viscous flow solutions
D)
Panel method and advanced viscous flow solutions

Correct Answer :   Panel method and advanced viscous flow solutions


Explanation : The numerical methods used were like source and vortex panel methods and numerical predictions of the viscous flow behavior, to analyze skin friction and flow separation effects. This was followed by experimental testing for verification of computer results.