** RAE602 AD-1 Syllabus**

AKTU Aeronautical Engineering(AE) RAE602 AD-1 Syllabus for all 5 units are provided below. Download link for AE 6th SEM RAE602 Aerodynamics-I Syllabus is listed down for students to make perfect utilization and score maximum marks with our study materials.

UP Technical University Aeronautical Engineering(AE) 6th SEM RAE602 AD-1 Aerodynamics-I Syllabus

**RAE 602: AERODYNAMIC-I**

**UNIT-1 **

Two Dimensional Ideal Fluid Flow: Continuity and momentum equations, Linear and angular

deformations, angular velocity, Circulation and vorticity. Irrotational flows. Stream and potential

functions. Varies flow as uniform flows, sources, sink, vortex flows and doublet flow. Kelvin

Theorem. Kutta-Joukow-ski theorem for lift. Aerodynamic forces. Types of Airfoils and their

Nomenclature.

**UNIT-2**

Complex Potential: Its properties and applications to various flows such as vortex doublet,

corner flow, full and half body Rankin, stationery and rotating cylinder. General expressions for

lift and Drag on body According to Blasius Theorem. Types of Vortex, interaction and

superimpose of vortices. Induced velocity due to vortices interaction. Mapping of flow fields.

Determination of pressure and velocity distributions on airfoil. Joukow-ski transformation

theorem. Joukow-ski transformation of circles into Circular arcs, elliptical airfoil, Symmetrical

and cambered airfoils.

**UNIT-3**

Thin Airfoil Theory (2-D Wing theory): Circulation and the generation of Lift and on thin

airfoil, Kutta condition on thin airfoil, thin airfoil theory, Lift and pitching moment coefficient of

flat and curved plates andairfoils. Effects flap on aerodynamic coefficients. Determination of

mean camber line, shapes for uniform and linear distribution of circulation. Bound vortex and

starting vortex, Downwash and induced drag. Helmholtz’s theorems. Aerodynamic center and

center of pressure.

**UNIT-4**

3-D Wings Theory- Vortex system around wing, horse shoe vortex. Helmholtz’s theorems. Biot

Savart’s law, Induced velocity (Downwash) of infinite, semi-infinite and finite filaments.

Prandtl’s classical lifting line theory, fundamental equations, elliptic lift distribution, influence of

aspect ratio on lift and drag, drag polar and lift correlation to aspect ratio. Techniques for general

span wise distribution, calculation of lift and vortex induced drag, numerical problems based on

above. Panel methods: General description of the panel methods.

**UNIT-5**

Viscous Flow Theory: Navier- Stroke’s equations, Exact solutions, Poiseulle flow and Cociette

flow. Velocity, tress and pressure distribution of their flows. Boundary layer theory. Blasius

solution of laminar flow. Laminar and turbulent boundary layers. Boundary layer separation and

control. Suction, blowing of Laminar flow Boundary layer thickness and momentum thickness of

laminar and turbulent. Safe factor, average skin friction coefficients and Drag force due to skin

friction coefficients.

**Books and References:**

1. E.L. Houghton and A.E. Brock, Aerodynamics for Engineering Students.

2. W.F. Durand (Editore), Aerodynamics Theory, Vols. I to VI, Dover Publications, 1963.

3. A.H. Shapiro, Dynamics and Thermodynamics of Compressible Flow Volts. I & II

Ronald Press 1953.

4. John D. Anderson, Fundamentals of Aerodynamics.

5. A. Ferri, Elements of Aerodynamics of Supersonic Flow, MacMillan, 1949.

6. D.O. Dommasch, S.S. Sherby & T.F. Connolly, Airplane Aerodynamics, Sir,

7. A.M. Kuethe& J.D. Schetzer, Foundations of Aerodynamics, Wiley, 1961.

8. L.N. Milne Thomson, Theoretical Aerodynamics, MacMillan, 1966.

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