About this document
Leishman 1990 by mostafakhazaee.peyman is a document available to read on EtoBox.
This document details an experimental investigation of the dynamic stall characteristics of a NACA 23012 aerofoil at a Reynolds number of 1.5 million. The study found that dynamic stall occurs through leading edge separation and involves complex fluid mechanics, including vortex shedding and pressure wave formation. The research aims to enhance understanding of unsteady aerodynamics and support the validation of theoretical models for dynamic stall phenomena.
- Author
- mostafakhazaee.peyman
- Language
- EN