M
Mitsuhiro Murayama
Researcher at Japan Aerospace Exploration Agency
Publications - 93
Citations - 2300
Mitsuhiro Murayama is an academic researcher from Japan Aerospace Exploration Agency. The author has contributed to research in topics: Drag & Wind tunnel. The author has an hindex of 21, co-authored 93 publications receiving 1934 citations.
Papers
More filters
Journal ArticleDOI
Efficient Optimization Design Method Using Kriging Model
TL;DR: The present method is applied to a two-dimensionalAirfoil design and the prediction of flap’s position in a multi-element airfoil, where the lift-to-drag ratio (L/D) is maximized.
Journal ArticleDOI
Summary of Data from the Fifth Computational Fluid Dynamics Drag Prediction Workshop
David W. Levy,Kelly R. Laflin,Edward N. Tinoco,John C. Vassberg,Mori Mani,Ben Rider,Christopher L. Rumsey,Richard A. Wahls,Joseph H. Morrison,Olaf Brodersen,Simone Crippa,Dimitri J. Mavriplis,Mitsuhiro Murayama +12 more
TL;DR: This workshop focused on force/moment predictions for the NASA Common Research Model wing-body configuration, including a grid refinement study and an optional buffet study.
Proceedings ArticleDOI
Summary of Data from the Fifth AIAA CFD Drag Prediction Workshop
David W. Levy,Kelly R. Laflin,Edward N. Tinoco,John C. Vassberg,Mori Mani,Ben Rider,Christopher L. Rumsey,Richard A. Wahls,Joseph H. Morrison,Olaf Brodersen,Simone Crippa,Dimitri J. Mavriplis,Mitsuhiro Murayama +12 more
TL;DR: Results from the 5, AIAA CFD Drag Prediction Workshop are presented, focused on force/moment predictions for the NASA Common research wing-body configuration, including a grid refinement study and an optional buffet study.
Journal ArticleDOI
Grid Quality and Resolution Issues from the Drag Prediction Workshop Series
Dimitri J. Mavriplis,John C. Vassberg,Edward N. Tinoco,Mori Mani,Olaf Brodersen,Bernhard Eisfeld,Richard A. Wahls,Joseph H. Morrison,Tom Zickuhr,David W. Levy,Mitsuhiro Murayama +10 more
TL;DR: In this paper, the effect of grid resolution and grid quality on aerodynamic drag prediction has been examined in detail and recommendations for improvements in mesh generation technology which have the potential to impact the state-of-the-art of aerodynamic prediction are given.
Proceedings ArticleDOI
Experimental Study of Slat Noise from 30P30N Three-Element High-Lift Airfoil in JAXA Hard-Wall Low-Speed Wind Tunnel
Mitsuhiro Murayama,Kazuyuki Nakakita,Kazuomi Yamamoto,Hiroki Ura,Yasushi Ito,Meelan M. Choudhari +5 more
TL;DR: Aeroacoustic measurements associated with noise radiation from the leading edge slat of the canonical, unswept 30P30N three-element high-lift airfoil configuration have been obtained in a 2 m x 2 m hard-wall wind tunnel at the Japan Aerospace Exploration Agency (JAXA) as discussed by the authors.