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Tetsuya Kunimasu

Observed names: KUNIMASU, Tetsuya, Kunimasu, Tetsuya, T. Kunimasu, Tetsuya KUNIMASU
OpenAlex ID: A5077257153
Boundary-Layer Transition Detection in a Cryogenic Wind Tunnel Using Luminescent Paint
1997 · Keisuke Asai, Hiroshi Kanda, et al. · Journal of Aircraft · 62
Anodized aluminum pressure sensitive paint in a cryogenic wind tunnel
1999 · Hirotaka Sakaue, John P. Sullivan, et al. · 45
Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint
1996 · Keisuke Asai, Hiroshi Kanda, et al. · AIAA Aerodynamic Measurement Technology and Ground Testing Conference · 24
Development of a 60cm Magnetic Suspension System.
2002 · Hideo Sawada, Tetsuya Kunimasu · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 22
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Cryogenic pressure sensitive fluorescent paint systems
1998 · Keisuke Asai, Hiroshi Kanda, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 15
Rolling Moment Control at the JAXA 60 cm MSBS
2005 · Hideo Sawada, Tetsuya Kunimasu, et al. · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 9
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Drag coefficients of cylinders magnetically supported in axial flow
2004 · Hideo Sawada, Hiroshi Higuchi, et al. · Journal of Wind Engineering · 9
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Sphere Drag Measurements with the NAL 60cm MSBS
2004 · Hideo SAWADA, Tetsuya KUNIMASU, et al. · Journal of Wind Engineering · 9
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Control Constants Decision Method of Proportional-Integral Control and Double Phase Advance for Magnetic Suspension and Balance Systems
2005 · Shinichi Suda, Hideo Sawada, et al. · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 7
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Pressure fluctuation measurements in the NAL 0.2-m supersonic wind tunnel
1998 · Hideo Sawada, Takashi Kohno, et al. · AIAA Aerospace Sciences Meeting and Exhibit · 7
Untitled
2007 · Hideo SAWADA, Tetsuya KUNIMASU, et al. · Journal of Wind Engineering · 5
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5-Axis Force Calibration Test Results for the JAXA 60cm MSBS
2004 · Hideo Sawada, Tetsuya Kunimasu, et al. · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 5
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A Magnetic Balance with Hall Effect Sensors
2004 · Hideo Sawada, Tetsuya Kunimasu, et al. · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 3
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Visualization of the quiet test region in a supersonic wind tunnel using luminescent paint
2002 · K. Asai, T. Kunimasu, et al. · International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF) · 3
Untitled
2008 · Hideo SAWADA, Hiroshi HIGUCHI, et al. · Journal of Wind Engineering · 2
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Magnetic Suspension of an AGARD-B Model in 6 D.O.F.
2006 · Hideo Sawada, Shinichi Suda, et al. · JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES · 2
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Non-intrusive measurements of a blunt circular cylinder in a magnetic suspension wind tunnel
2008 · Hideo Sawada, Hiroshi Higuchi, et al. · Journal of Wind and Engineering · 1
519 Analysis on Control Characteristics of Magnetic Suspension and Balance System for High Subsonic Wind Tunnel
2004 · Shinichi SUDA, Hideo SAWADA, et al. · The Proceedings of the Dynamics & Design Conference · 1
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6:1 Axial-Symmetric Ellipsoid Drag Measurement with a Magnetic Suspension Balance System
2003 · Hideo SAWADA, Tetsuya KUNIMASU, et al. · Journal of Wind Engineering · 1
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The NAL 0.2 m supersonic wind tunnel
1996 · Hideo Sawada, Koichi Suzuki, et al. · JAXA Repository (JAXA) · 1
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Sting-free Unsteady Flowfield, Base Pressure and Force Measurements on Axisymmetric Bluff-Body
2006 · Hiroshi Higuchi, Hideo Sawada, et al. · APS Division of Fluid Dynamics Meeting Abstracts
PIV Measurements of Magnetically Suspended Circular Cylinder in Axial Air Stream
2006 · Hiroyuki KATO, Hiroshi HIGUCHI, et al. · Journal of the Visualization Society of Japan
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セッシュン6 (8編) 基本断面の空力特性
2005 · Masaru MATSUMOTO, Hiromichi SHIRATO, et al. · Wind Engineers JAWE
低温環境におけるジャッキ装置耐久試験:0.2m超音速風洞可変ノズル制御用ジャッキ装置について
2004 · Tetsuya Kunimasu, Hideo Sawada, et al. · JAXA Repository (JAXA)
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低温環境におけるジャッキ装置耐久試験:0.2m超音速風洞可変ノズル制御用ジャッキ装置について
2004 · 国益, 徹也, 澤田, 秀夫, et al. · Institutional Repositories DataBase (IRDB)
Works count: 45
Citation count: 233
H-index: 8
I10-index: 5
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