Aerodynamics research on micro air vehicles

Zhan Ke Li, Bi Feng Song, Ya Feng Zhang

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

In the paper, Based on the low Reynolds number aerodynamics of the micro air vehicles (MAVs), some researches were done, such as aerodynamics characteristic numerical analysis research on the airfoil at low Reynolds numbers, numerical calculation method of low Mach low Reynolds numbers fluid field, estimation method research on aerodynamic characteristic of the aeroelastic flapping wing, unsteady vortex method of aerodynamics characteristic estimation and wind tunnel test of MAVs. The results of this paper have important reference value and instructive meaning to the development of MAVs.

Original languageEnglish
Pages (from-to)137-141
Number of pages5
JournalXitong Gongcheng Lilun yu Shijian/System Engineering Theory and Practice
Volume25
Issue number9
StatePublished - Sep 2005

Keywords

  • Flapping wing
  • Micro air vehicles (MAVs)
  • Reynolds number
  • Wind tunnel test

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