filmov
tv
thin airfoil theory panel code unsteady aerodynamics
Показать описание
This animation has been created for course AE4135 Rotor Wake Aerodynamics at TU Delft, Aerospace Engineering MSc program.
The video shows the unsteady aerodynamic respons for an oscillating airfoil at reduced frequency k=0.1 (unsteady domain).
Programmed in Matlab, based on Katz & Plotkin Aerodynamics chapter 13.
The video shows the unsteady aerodynamic respons for an oscillating airfoil at reduced frequency k=0.1 (unsteady domain).
Programmed in Matlab, based on Katz & Plotkin Aerodynamics chapter 13.
0:00:14
thin airfoil theory panel code unsteady aerodynamics
0:00:22
Thin airfoil panel code pitching flowfield
0:23:36
Thin airfoil theory [Aerodynamics #12]
0:22:35
Airfoil Analysis . Thin Airfoil Theory . Fundamental Equation
0:09:06
Airfoil Analysis . Thin Airfoil Theory . Infinite-Series Solution
0:03:53
Thin Airfoil Theory - Kutta Condition
0:23:19
Airfoil Analysis . Thin Airfoil Theory . Example Application
![[Aerodynamics] A History](https://i.ytimg.com/vi/txjGmtknCOg/hqdefault.jpg)
0:29:42
[Aerodynamics] A History of Aerodynamics, Part 3, the Age of Fruition in theoretical aerodynamics
0:21:39
Airfoil Analysis . Thin Airfoil Theory . Small-Angle Pitching Moment
0:16:14
Airfoil Analysis . Vortex Panel Method . Algorithm Outline
1:03:24
Thin Airfoil Theory
0:17:40
Airfoil Analysis . Vortex-Panel Method with Integral Boundary Layer . Methodology Overview
0:16:45
Airfoil Analysis . Vortex Panel Method . Development
0:11:21
Airfoil Analysis . Vortex Panel Method . Influence Matrix
0:00:27
Case 3A - Animation
0:24:54
Panel methods [Aerodynamics #11]
0:00:33
2D Unsteady Discrete Vortex Method (inertial frame)
0:00:07
heaving motion of a naca airfoil - 3D Unsteady panel method
0:08:42
Airfoil Analysis . Vortex Panel Method . Forces and Moments
0:07:33
Airfoil Analysis . Camber-Line Design . Example Uniform Load
0:08:15
Fundamentals of Aerodynamics . Superposition of Potential Flows . Vortex Panel
0:15:08
Vortex Panel Method: Airfoil
0:09:23
Vortex Panel Method: System of Equations
0:08:54
Finite Wings . Introduction . Basic Principles
Комментарии