AERONAUTICAL ENGINEERING
UNIT-I INTRODUCTION
TO LOW SPEED FLOW
Models of the
fluid: control volumes and fluid elements. Continuity, Momentum and energy equations.
Substantial derivative, Vorticity and circulation, stream function,
irrotational flow, velocity potential, Euler equation, incompressible
Bernoulli’s equation.
UNIT-IITWO
DIMENSIONAL INVISCID INCOMPRESSIBLE FLOW
Laplace
Equation, Elementary flows and their combinations, Ideal Flow over a circular
cylinder, Alembert’s paradox, Magnus effect, Kuttajoukowski’s theorem, real
flow over smooth and rough cylinder
UNIT-III AIRFOIL THEORY
Cauchy-Riemann relations, complex potential, methodology of
conformal transformation, Kutta-Joukowski transformation and its applications, Kuttacondition, kelvin’scirculation theorem, starting vortex, thin airfoil theory and
its applications.
UNIT-IV WING THEORY
Vortex filament, Biot-savart law, Helmholtz Theorems bound
vortex and trailing vortex, horse shoe vortex, lifting line theory and its
limitations.
UNIT-V VISCOUS FLOW
Newton’s
law of viscosity, Boundary Layer, Navier-Stokes equation, displacement,
Momentum thickness, Flow over a flat plate, Blasius solution.
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