School of Aeronautics (Neemrana) provides platform and environment for open discussions and interactions between the faculty and students and is designed to ignite and serve the urge to explore and learn beyond boundaries.
This would enable the students to discover, nurture and expand their individual talents, skills and interests so that they emerge as leaders in path breakers wherever they go.
This blog has been created with a view where staff and students can share their latest updates regarding various Technical & General Subjects / Topics, category wise
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
