Browse > Article

Propeller Design of Unmanned Target Drone for the Performance Improvement  

Lee Sangmyeong (인하대학교 항공우주공학과)
Sung Hyunggun (인하대학교 항공공학과)
Roh Taeseong (인하대학교 항공공학과)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.9, no.1, 2005 , pp. 46-52 More about this Journal
Abstract
A propeller as a propulsion system has been redesigned to improve performance of a target drone. The vortex theory has been applied for the propeller design method. Design variables have been the chord length along the direction of blade radius, the change of blade radius, and the geometric angle of the blade. The existing propeller has been redesigned and modified considering engine RPM change to get the improved thrust at both low and high speeds.
Keywords
Unmanned Target Drone; Propeller; Vortex Theory; Gear-Reduction; RPM; Chord Length; Pitch Angle;
Citations & Related Records
연도 인용수 순위
  • Reference