There are following steps to do CFD (Computational Fluid Dynamics) analysis of F-16 Fighter falcon are:-
STEP-1 MODELLING AND ENCLOSURE
STEP-2 MESHING AND SELECTION OF INLET AND OUTLET VELOCITY PASSAGE
STEP-3 INPUT PARAMETER AND CONDITIONS
Boundary condition:-
viscosity:- K-epsilon (2-equation)
STEP-4 RUN ITERATIONS AND PLOT THE GRAPHSTEP-5 EFFECT OF PRESSURE
STEP-6 EFFECT OF VELOCITY
At Y-axis
At Z-axis
Presented by :- Er. Saurabh Malpotra