Enhancing Propeller Performance Through Design Modifications: A Study on Ridged Propeller Design

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Authors: Panduranga Rohith Dacharla
Cited by: 0

Abstract

This study analyzes a Ridged Propeller design using computational simulations to assess improvements in lift and turbulence compared to a conventional propeller. Three design versions (V1, V2, V3) were evaluated at a fixed RPM. The results show consistent lift enhancement and turbulence reduction across all versions. The findings highlight the aerodynamic benefits of ridge-based blade modifications for improving propeller performance in UAV and aerospace applications.

Fields of Study & Subjects

Computational Fluid Dynamics and Aerodynamics Fluid dynamics and aerodynamics studies Aerospace and Aviation Technology

Publication details

Journal / source
Journal of Aerospace Sciences and Technologies
Pages
1–16
Publication date
23 February 2026
Language
EN