Skip to content

Commit ec50b57

Browse files
committed
docs: fix PANKH acronym expansion in README (of → for)
1 parent d3bcbee commit ec50b57

File tree

1 file changed

+1
-1
lines changed

1 file changed

+1
-1
lines changed

README.md

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -13,7 +13,7 @@
1313

1414

1515
## Description
16-
This project implements **PANKH** (Panel Analysis of uNsteady Kinematics of Hovering airfoils), a solver designed to study the aerodynamics of flapping foils. PANKH is a **low-fidelity solver** that solves the **Laplace equation** to determine the velocity distribution in the flow field. It enforces the **Neumann boundary condition** to satisfy the **no-penetration condition** (zero normal flux) on the airfoil surface. The **unsteady Bernoulli equation** is then applied to compute the pressure difference across the airfoil, enabling the calculation of aerodynamic loads.
16+
This project implements **PANKH** (Panel Analysis for uNsteady Kinematics of Hovering airfoils), a solver designed to study the aerodynamics of flapping foils. PANKH is a **low-fidelity solver** that solves the **Laplace equation** to determine the velocity distribution in the flow field. It enforces the **Neumann boundary condition** to satisfy the **no-penetration condition** (zero normal flux) on the airfoil surface. The **unsteady Bernoulli equation** is then applied to compute the pressure difference across the airfoil, enabling the calculation of aerodynamic loads.
1717

1818
![Vortex shedding animation](JOSS/vortex_shedding.gif)
1919

0 commit comments

Comments
 (0)