About this document
Propeller Design for Antonov AN-32 by md.shamsul arifin is a document available to read on EtoBox.
This document presents a design for a new propeller for the Antonov AN-32 aircraft to improve efficiency and performance. It analyzes the different types of propellers and selects a constant speed propeller. The design process involves selecting airfoil profiles for the root, mid, and tip sections and using blade element momentum theory calculations. Preliminary calculations are presented to determine parameters like advance ratio and tip speed. The results from the calculations in Matlab are presented in a
- Author
- md.shamsul arifin
- Language
- EN