Course Name: AS5010 : Engg. Aerodyn. & Flt. Mech.

Description: Basic equations of Fluid Mechanics. Inviscid flows. Stream function. Velocity potential. Twodimensional incompressible flows: Lapalce's equation, its solutions. Flow over airtfoils? Conformal transformation, thin airfoil theory. Introduction to finite wings? Prandtl's lifting line theory. Effect of boundary layer and separation on flow over airfoils. Atmosphere. Estimation of basic performance of an airplane. Introduction to stability and control.

Slot: D

RoomNo: CR4

Instructor: Sameen A

Period: JUL-NOV 2013

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