Subject Details
Dept     : AERO
Sem      : 6
Regul    : R2019
Faculty : N.Venkatesh
phone  : NIL
E-mail  : venkat.n.aero@snsct.org
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Lecture Notes

UNIT 1:
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Mathematical properties of Fluid Dynamics Equations ‐ Elliptic, Parabolic and Hyperbolic
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Discretization
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Explicit finite difference
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Grid generation – Introduction, types of grids
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Source panel method ‐ Vortex panel method
UNIT 2:
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Stability properties of explicit and implicit methods
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‐ Concept of numerical dissipation
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Boundary layer equations and methods of solution
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Further advantages of upwind differencing.
UNIT 3:
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Finite Element Techniques in Computational Fluid Dynamics
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Implementation of the FEM ‐ The solution procedure.
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Piecewise defined shape functions;
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‐ Weighted residual formulation ‐Galerkin formulation
UNIT 4:
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Lax – Wendroff time stepping, Runge‐Kutta time Stepping ‐ Multi‐stage time stepping
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Lax – Wendroff time stepping, Runge‐Kutta time Stepping ‐ Multi‐stage time stepping
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Finite Volume Techniques ‐ Cell centered formulation
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Accuracy Cell vertex formulation
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FDM ‐like finite volume techniques
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Central and up‐wind type discretization
UNIT 5:
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Pressure and Velocity corrections
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Pressure correction equation; SIMPLE algorithm and its variants
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PISO algorithms; Turbulence models – algebraic mixing length model, one and two equation models
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Case study of Stage separation Aerodynamics of future space transport systems
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CFD models utilizing algebraic mixing length models