Flow visualization of wake of a quad-copter in ground effect

Hikaru Otsuka, Masayoshi Kohno, Keiji Nagatani

Research output: Contribution to conferencePaper

Abstract

The wake flow of a small quadcopter unmanned aerial vehicle generates a ground effect during take-off and landing. The ground effect affects the rotor thrust and posture stability. However, the structure of the wake with plural rotors has not been unveiled experimentally. In this study, the wake flow structure of a quadcopter with flow interaction between rotors was examined, and the wakes of hovering were visualized using a laser light sheet. In addition, particle image velocimetry measurements were conducted, changing ground off height and the distance between rotors. The visualization results in several planes suggested a merging wake between rotors and pulled wake at the center of the quadcopter. Furthermore, the particle image velocimetry results showed the development of a soaring flow at the center of the quadcopter in the ground effect operation, and the velocity of the soaring flow decelerated with closing rotor distance. The experimental results indicate that the soaring flow pushes the quadcopter; this flow affects the lifting force on the quadcopter during the ground effect.

Original languageEnglish
Publication statusPublished - 2017 Jan 1
Event6th Asian-Australian Rotorcraft Forum and Heli Japan 2017, ARF 2017 - Kanazawa, Ishikawa, Japan
Duration: 2017 Nov 72017 Nov 9

Other

Other6th Asian-Australian Rotorcraft Forum and Heli Japan 2017, ARF 2017
CountryJapan
CityKanazawa, Ishikawa
Period17/11/717/11/9

ASJC Scopus subject areas

  • Aerospace Engineering
  • Instrumentation
  • Electrical and Electronic Engineering
  • Control and Systems Engineering

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