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 GRAPH
STEP-5 EFFECT OF PRESSURE

STEP-6 EFFECT OF VELOCITY
At Y-axis

At Z-axis

Presented by :- Er. Saurabh Malpotra