Yoshine Ueda

Natural laminar flow wing for supersonic conditions: Wind tunnel experiments, flight test and stability computations

Olivier Vermeersch, Kenji Yoshida, Yoshine Ueda et al. · Progress in Aerospace Sciences · 2015 · 26 citations

Aerodynamic Testing, Unsteady Flow, Aeronautics +9

Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions

Yoshine Ueda, Kenji Yoshida, Kisa Matsushima et al. · AIAA Journal · 2014 · 26 citations · Full text

Wing Design, Aeroacoustics, Unsteady Flow +15

Pressure Gradient Effects on Supersonic Transition over Axisymmetric Bodies at Incidence

Naoko Tokugawa, Meelan M. Choudhari, Hiroaki Ishikawa et al. · AIAA Journal · 2015 · 22 citations

Flow Control, Engineering, Fluid Mechanics +17

CFD Validation Study for a High-Lift Configuration of a Civil Aircraft Model

Mitsuhiro Murayama, Yuzuru Yokokawa, Kazuomi Yamamoto et al. · 25th AIAA Applied Aerodynamics Conference · 2007 · 22 citations

Aeronautics, Engineering, Aerospace Engineering +11

Transition Measurement of Natural Laminar Flow Wing on Supersonic Experimental Airplane NEXST-1

Naoko Tokugawa, Dong-Youn Kwak, Kenji Yoshida et al. · Journal of Aircraft · 2008 · 19 citations

Aerodynamic Design Conditions, Transition Locations, Aeronautics +10