Subject Details
Dept     : AERO
Sem      : 4
Regul    : 2019
Faculty : Ramesh M
phone  : NIL
E-mail  : ramesh.m.aero@snsct.org
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Lecture Notes

UNIT 1:
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Introduction to basic Aerodynamics, Continuity equation
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Momentum & energy equations
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Aerodynamic forces and Moments
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Viscous flow - Newton‘s law of viscosity- Viscous boundary layer
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Methods to delay Flow Separation Flow over a flat plate, Blasius solution – Navier Stokes equation
UNIT 2:
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Airfoils Nomenclature and NACA series - Airfoil Characteristics
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Vortex sheet - Kelvin Circulation theorem - Thin aerofoil theory and its applications
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Introduction to Finite wing - Downwash and Induced Drag
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Biot Savart law and Helmhotz‘s theorems - Horse shoe vortex
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Prandtl‘s Classical Lifting line theory and its limitations
UNIT 3:
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Prandtl equation and Rankine Hugoniot relation
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Normal shock equations - Pitot static tube, corrections for subsonic and supersonic flows
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Normal shock equations - Pitot static tube, corrections for subsonic and supersonic flows
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Rayleigh and Fanno Flow – Flow past convex corners
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Expansion hodograph - Reflection and interaction of shocks and expansion waves