Measurement of differential pressure on a butterfly wing

Hidetoshi Takahashi, Kiyoshi Matsumoto, Isao Shimoyama

研究成果: Conference contribution

11 被引用数 (Scopus)

抄録

This paper reports on direct measurement of differential pressure on a butterfly wing during free flight. Differential pressure was measured using a micro-fabricated sensor. A piezo-resistive cantilever was used as a differential pressure sensor. The sensor was 1.0 mm x 1.0 mm x 0.3 mm in size and 0.7 mg in weight so that it did not interfere with wing motion. By attaching the sensor to the center of a butterfly forewing with a flexible wiring, the differential pressure on the wing was measured during "no flight flapping" and "taking off".

本文言語English
ホスト出版物のタイトルMEMS 2010 - The 23rd IEEE International Conference on Micro Electro Mechanical Systems, Technical Digest
ページ63-66
ページ数4
DOI
出版ステータスPublished - 2010 6 1
外部発表はい
イベント23rd IEEE International Conference on Micro Electro Mechanical Systems, MEMS 2010 - Hong Kong, China
継続期間: 2010 1 242010 1 28

出版物シリーズ

名前Proceedings of the IEEE International Conference on Micro Electro Mechanical Systems (MEMS)
ISSN(印刷版)1084-6999

Other

Other23rd IEEE International Conference on Micro Electro Mechanical Systems, MEMS 2010
国/地域China
CityHong Kong
Period10/1/2410/1/28

ASJC Scopus subject areas

  • 電子材料、光学材料、および磁性材料
  • 凝縮系物理学
  • 機械工学
  • 電子工学および電気工学

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