Constant Source Panel Method

Specifically, we look at the

Lecture 14 - Source Panel Method (3/01/2021)

After solving for the geometric integral from the previous video (Iij), we have the expression for the normal velocity on a

In this video, we will combine the

Source panel method

In the previous video (Building More Complex Flows), we ended with an equation for the velocity potential induced at an arbitrary ...

Surface pressure distribution about 2d non-lifting surfaces using surface distribution

Flows over a circular cylinder are a bit boring, so here we apply the same code (with a couple minor tweaks) to the flow over an ...

This is the first real step towards writing a

In this video, I explain the steady

Derivation of how to implement a Hess/Smith

Here we are. We finally have all the mathematical information needed to code up the

...

Course Name : Fundamentals of Theoretical and Experimental Aerodynamics Subject : Aerospace Engineering Welcome to ...

Here I go over the vortex paneling

Describes the

In the previous video (Flow Around an Airfoil), we ended with an expression that still needed some simplification before we could ...