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Calculating circulation for flat plate
Lesson 16 of 20 • 1 upvotes • 14:57mins
Shantanu Kandwal
Coefficient of lift and moment for 1) flat plate 2) cambered airfoil. Not fully derived but from gate point of view everything is covered. For more detail refer to textbook.
Aerodynamics of subsonic flows for GATE
20 lessons • 4h 13m
1
Rudimentary Flow Over Flat Plate
10:22mins
2
Mathematical Tools
12:41mins
3
Fundamental Equation of Aerodynamics
13:56mins
4
The Momentum Equation
12:09mins
5
Rotational Flows, Facts about Boundary Layer
11:31mins
6
Energy equation.
14:29mins
7
Energy equation
14:29mins
8
Difference between eulerian and lagrangian
14:17mins
9
Circulation and its physical significance.
13:13mins
10
Pathlines, Streamline and streaklines.
14:04mins
11
Pitot-static tube.
11:33mins
12
Elementary Flows
8:31mins
13
Doublet flows + uniform flow
10:53mins
14
Vortex flows: lifting flow around cylinder
13:01mins
15
Incompressible flow around airfoils.
14:54mins
16
Calculating circulation for flat plate
14:57mins
17
Aerodynamic center
10:36mins
18
3-D flow over a finite wing.
12:08mins
19
Continued: Prandlt Lifting Line theory
12:30mins
20
General lift distribution.
12:47mins
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