Fluid Mechanics and Flight Mechanics

Theoretical model and experiment on rotor in finite ground effect

  • XIN Ji ,
  • LI Pan ,
  • CHEN Renliang ,
  • LIU Dawei
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  • 1. General Designing Department, China Helicopter Research and Development Institute, Jingdezhen 333001, China;
    2. National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
    3. School of Aeronautic Science and Engineering, Beihang University, Beijing 100083, China

Received date: 2016-03-14

  Revised date: 2016-07-25

  Online published: 2016-08-22

Supported by

National Natural Science Foundation of China (51405227)

Abstract

A new flow-field analysis model for the finite ground effect of the rotor is developed. Considering the complexity of the ground effect caused by finite ground, a "material line" rectification method is proposed to solve the problem that part of wake vortices may non-physically "penetrate" the finite ground in discrete prediction, and a high stability time-stepping free-wake algorithm with 3rd-order accuracy is introduced into the model. Considering the shortage of existing experimental data for finite ground effect, a finite ground effect experiment research is also implemented, and the thrust, torque and flap angle of a hovering and flying rotor are measured. The experimental data validates the analysis model proposed in this paper. According to the wake geometry got from theoretical model, several flying states of rotor in finite ground effect are analyzed, and some reasonable conclusions are gained.

Cite this article

XIN Ji , LI Pan , CHEN Renliang , LIU Dawei . Theoretical model and experiment on rotor in finite ground effect[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017 , 38(3) : 120219 -120219 . DOI: 10.7527/S1000-6893.2016.0221

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