TY - GEN
T1 - Aerodynamic Hysteresis and Reynolds Number Effect of Slanted Cylinder Afterbody in Magnetic Suspention and Balance System
AU - Tashiro, Kodai
AU - Yokota, Sho
AU - Zigunov, Fernando
AU - Ozawa, Yuta
AU - Nonomura, Taku
AU - Asai, Keisuke
N1 - Funding Information:
This work was supported by JSPS KAKENHI Grant Numbers JP19KK0116 and JP21H04586.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - 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.
AB - 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.
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U2 - 10.2514/6.2022-4167
DO - 10.2514/6.2022-4167
M3 - Conference contribution
AN - SCOPUS:85135233420
SN - 9781624106354
T3 - AIAA AVIATION 2022 Forum
BT - AIAA AVIATION 2022 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA AVIATION 2022 Forum
Y2 - 27 June 2022 through 1 July 2022
ER -