B.Tech III Year II Semester (R18)
Introduction to computational aerodynamics, the major theories, approaches and methodologies used in computational aerodynamics. Applications of computational aerodynamics for classical aerodynamic‘s problems.
Introduction to gambit, geometry creation, suitable meshing types and boundary conditions.
Introduction to fluent, boundary conditions, solver conditions and post processing results.
Flow over a flat plate at low Reynolds numbers, observe the boundary layer phenomena, no slip condition and velocity profile inside the boundary layer.
Flow through pipe at different Reynolds numbers; observe the velocity changes for laminar and turbulent flows.
Flow over a circular cylinder at different Reynolds numbers, observe the properties at separation region and wake region.
Flow over a cambered aerofoil at different velocities, observe flow properties and compare the computation results with experimental results (consider the model from aerodynamics laboratory).
Flow over a symmetric aerofoil at different velocities, observe flow properties and compare the computation results with experimental results (consider the model from aerodynamics laboratory).
R18 B.TECH AERONAUTICAL ENGG. III YEAR
Flow over wedge body at supersonic mach number; observe the shock wave phenomena and change of properties across the shock wave.
Flow over a cone at supersonic mach number; observe the shock waves and 3D relieving effect.
Solution for the following equations using finite difference method I. One dimensional wave equation using explicit method of lax. II. One dimensional heat conduction equation using explicit method.
Generation of the following grids I. Algebraic grids. II. Elliptic grids.
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