Aerodynamic Hysteresis and Reynolds Number Effect of Slanted Cylinder Afterbody in Magnetic Suspention and Balance System

Kodai Tashiro, Sho Yokota, Fernando Zigunov, Yuta Ozawa, Taku Nonomura, Keisuke Asai

研究成果: Conference contribution

抄録

A test model called slanted cylinder afterbody was magnetically supported by a magnetic suspension and balance system (MSBS) in this wind tunnel test. The stability of the levitation was found to be accurate to less than 8.9 m and 18.6 mdeg at 15 m/s freestream. The aerodynamic force on the model and the wake at the center plane in the streamwise direction were investigated. In the range of the diameter-based Reynolds number of 3.3 × 104 − 3.6 × 104, the flow around the model was critically changed.

本文言語English
ホスト出版物のタイトルAIAA AVIATION 2022 Forum
出版社American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624106354
DOI
出版ステータスPublished - 2022
イベントAIAA AVIATION 2022 Forum - Chicago, United States
継続期間: 2022 6月 272022 7月 1

出版物シリーズ

名前AIAA AVIATION 2022 Forum

Conference

ConferenceAIAA AVIATION 2022 Forum
国/地域United States
CityChicago
Period22/6/2722/7/1

ASJC Scopus subject areas

  • エネルギー工学および電力技術
  • 原子力エネルギーおよび原子力工学
  • 航空宇宙工学

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