I have to model a simple rectangular wing for my experimental aircraft testing a new technology on it. I have to choose an airfoil among the ten options given for my wing which would give the best aerodynamic performance. Suggest the best method to test and fix one airfoil.
(a) CFD analysis
(b) Literature
(c) Wind tunnel models
(d) Calculations
I got this question in an online interview.
Query is from CFD Advantages and Disadvantages in section Philosophy of Computational Fluid Dynamics of Computational Fluid Dynamics