Flow Control Group
Study on reduced-order model for optimal feedback control of dynamic stall flow
OKA, Yoshinori
Advanced Measurement Group
Visualization of pressure fluctuation of supersonic cavity flow by PSP measurement
KASAI, Miku
Advanced Measurement/Fluid Dynamics Group
Study of unsteady interference flow under compressible low Reynolds number conditions using pressure-sensitive paints
LEE, Chung Il
Advanced Measurement Group
Study on quantitative measurement of density field of supersonic jet by BOS method
Advanced Measurement Group
Elucidation of aerodynamic performance enhancement mechanism with active flow control device by using dual-luminophore PSP
VIGUERA, Rodrigo
Flow Control Group
Study on highly efficient fluid control using data-driven low-dimensional models
KANEKO, Sayumi
Advanced Measurement Group
TBD
KONG, Di
Advanced Measurement Group
Study on pressure field measurement of high-speed fluid phenomena using PSP
OKUIZUMI, Hiroyuki
(Doctoral course for working adults)
Fluid Dynamics Group
Investigation of flow over a rotating sphere using MSBS
HOSAKA, Tomoyuki
(Doctoral course for working adults)
Flow Control Group
Research Title: TBD
Alumni (Ph.D student)
FY2019
・MATSUI, Akitoshi: Wind Tunnel Testing Techniques for Trains to Assess Crosswind Stability and Evaluate Aerodynamic Noise with Noise Source Detection
FY2019
・Yuta Ozawa: Aeroacoustic Fields of Multiple Ideally Expanded Supersonic Jets of Mach Number of 2.0
・Takayuki Nagata: Study on Compressible Low-Reynolds-Number Flow over a Sphere
・LEE, Tekjin: Skin-Friction Field Measurements Using Luminescent Oil-Film Image Analysis
FY2018
・Yosuke Sugioka: Innovative Pressure-Sensitive Paint Techniques and Their Application to Unsteady Aerodynamics Studies in Aerospace Engineering
・TRAN, The Hung: An Experimental Study of the Effect of Boattail Angle on Flow Field and Drag of Axisymmetric Afterbodies at Low-Speed Condition
FY2017
・Takuro Daimaru: Numerical Analysis of Oscillating Heat Pipe (Because Nagai Lab became independent, he belonged to Nagai Lab when he got his degree.)
FY2014
・Koji Fujita: Studies on a Mars Airplane with Aerial Deployment Technique
FY2013
・Shohe Uramoto: ステレオPIVを用いた超音速境界層及び超音速噴射流れ場の乱れ構造に関する実験的研究
FY2011
・Daisuke Yorita: Development of High-Accuracy Pressure-Sensitive Paint Techniques and Their Applications to Low-Speed Unsteady Flow Phenomena
FY2010
・Masayuki Anyoji: Application of Molecular Sensors to Low-Speed Flow
FY2007
・Taro Tamashita: Application of Molecular Sensors to Low-Speed Flow
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