AE34O1 AERODYNAMIC 1

   


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      Santhosh (Admin) 
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UNIT I INTRODUCTION TO LOW-SPEED FLOW


Euler equation 2m

irrotational flow2 m

 incompressible Bernoulli's equation*** green's lemma 

Stoke's theorem, kelvin's theorem***

Equipotential lines, elementary flows and their combinations.


UNIT II TWO-DIMENSIONAL INVISCID INCOMPRESSIBLE FLOW


 magnus effect 2m


D'Alembert's paradox,***Suma also expected 

 Kutta Joukowski's theorem, Kutta condition***

, real flow over smooth and rough cylinder.


UNIT III AIRFOIL THEORY


Cauchy-Riemann relation

 Kutta- Joukowski transformation and its applications***

 thin airfoil theory and its applications***


UNIT IV SUBSONIC WING THEORY

Biot and Savart law****

 bound vortex and trailing vortex**

lifting line theory and its limitations.


UNIT V INTRODUCTION TO BOUNDARY LAYER THEORY


Boundary layer and boundary layer, displacement, energy thickness***

boundary layer equations for a steady

 two-dimensional incompressible flow, boundary layer growth over a flat plate***

Blasius solution, basics of turbulent flow. 2m or 8m


PART-C
1.Compulsory Questions {a case study where the student will have to read and analyse the subject }
A. May be a sum so study all algorithm properly to get good scores
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