Development of vertical takeoff and landing vehicle with flapping wings

Takeshi Sumita, Shun Takahashi, Norio Arai, Koji Shimoyama, Shinkyu Jeong, Shigeru Obayashi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Flying beings by flapping wings show a hovering flight without stall because they can exploit vortices for their flight. The mechanism of the flapping wing flight makes clear, gradually. Therefore, it is considered that a flapping wing vehicle can be developed based on the mechanism with high efficiency rather than fixed-wing aircraft and rotary-wing aircraft in some situation. However, the flapping motion of flying beings is too complicated to reproduce completely. In this paper, flowfields around simplified flapping motion for the real flapping vehicle are investigated using CFD to make clear the relationship between vortices and unsteady fluid forces. Moreover, several motion parameters to develop the vertical takeoff and landing (VTOL) aircraft with flapping motion are discussed based on the actual equipment.

Original languageEnglish
Title of host publication30th AIAA Applied Aerodynamics Conference 2012
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages2455-2467
Number of pages13
ISBN (Print)9781624101854
DOIs
Publication statusPublished - 2012
Externally publishedYes
Event30th AIAA Applied Aerodynamics Conference 2012 - New Orleans, LA, United States
Duration: 2012 Jun 252012 Jun 28

Publication series

Name30th AIAA Applied Aerodynamics Conference 2012

Other

Other30th AIAA Applied Aerodynamics Conference 2012
CountryUnited States
CityNew Orleans, LA
Period12/6/2512/6/28

ASJC Scopus subject areas

  • Aerospace Engineering

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