Media Summary: Simulation of a NACA4412 with the Aviumtechnologies Simulation of the Caradonna Tung rotor in hover with the Aviumtechnologies Pusan National University Applied Aerodynamic Design Laboratory.
Unstructured Panel Method Wing Tail - Detailed Analysis & Overview
Simulation of a NACA4412 with the Aviumtechnologies Simulation of the Caradonna Tung rotor in hover with the Aviumtechnologies Pusan National University Applied Aerodynamic Design Laboratory. Small demonstration video showing optimization flow of a simple tapered aircraft Free courses, more videos, practice exercises, and sample code available at Come check it out聽... UVLM with wake rollup following the procedure described in "Low Speed Aerodynamics" (Katz & Plotkin, 2001).
![Panel methods [Aerodynamics #11]](https://i.ytimg.com/vi/AGVG2K6R9GA/mqdefault.jpg)
