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Dive into the research topics where Kazuyasu Matsuo is active.

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Featured researches published by Kazuyasu Matsuo.


48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition | 2010

Quantitative Flow Visualization of Correctly Expanded Supersonic Jets by Rainbow Schlieren Deflectometry

Yoshiaki Miyazato; Masayuki Irie; Hideki Yamamoto; Kazuyasu Matsuo; Hibikino Wakamatsu-ku

A quantitative visual study of a correctly-expanded supersonic jet of a Mach number of 1.6 by the rainbow schlieren deflectometry has been conducted to reveal the jet flow field quantitatively. Rainbow schlieren images of the jet have been taken by a schlieren system with a rainbow filter which has a continuous hue distribution. The density contour plot of the jet flow is determined by using the image analysis based on the Abel inversion of experimental data of transverse displacement at the cut-off plane. Also, Pitot probe measurements at a jet cross-section have been carried out to obtain density profiles. The radial distribution of the density from the schlieren quantitatively agrees well with that from the Pitot probe.


49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 2011

Measurements in Overexpanded Supersonic Jets by Rainbow Schlieren Deflectometry

Yoshiaki Miyazato; Yuji Ishida; Hideki Yamamoto; Kazuyasu Matsuo; Hibikino Wakamatsu-ku

A visual study of an overexpanded supersonic jet issuing from an axisymmetric convergent-divergent nozzle by the rainbow schlieren deflectometry technique has been conducted to reveal the shock containing jet flow field quantitatively. Rainbow schlieren images of the jet have been taken by a schlieren system with a rainbow filter which has a continuous hue distribution. The density contour plot of the jet flow is determined by using the image analysis based on the Abel inversion of experimental data of transverse displacement at the cut-off plane. Leading and rear shocks as well as a Mach disk in the jet flow are clearly visible in the density contour plot of the jet. Also, the density ratio across the Mach disk obtained from the experiment shows an excellent agreement with the theoretical value across a normal shock wave quantitatively.


Jsme International Journal Series B-fluids and Thermal Engineering | 1997

Attenuation and distortion of a compression wave propagating in a high-speed railway tunnel

Shinya Mashimo; Eiji Nakatsu; Toshiyuki Aoki; Kazuyasu Matsuo


42nd AIAA Aerospace Sciences Meeting and Exhibit | 2004

A Preliminary Study on Acetone Laser-Induced Fluorescence Technique for Low Temperature Flows

Masashi Kashitani; Yutaka Yamaguchi; Taro Handa; Mitsuharu Masuda; Kazuyasu Matsuo


Archive | 1987

Visual studies of characteristics of slip stream in Mach reflection of a shock wave

Kazuyasu Matsuo; Toshiyuki Aoki; Hiroyuki Hirahara


KSME/JSME THERMAL and FLUID Engineering Conference | 1998

Ballast Effect on Attenuation and Distortion of Pressure Wave Propagating in High-Speed Railway Tunnel

Shinichiro Nakao; Toshiyuki Aoki; Kazuyasu Matsuo


The Proceedings of Conference of Chugoku-Shikoku Branch | 2011

1112 Experimental Study on Total Pressure Loss of Compressible Flow in Curved Pipes

Tsuyoshi Yasunobu; Yoshiaki Miyazato; Hideki Yamamoto; Kazuyasu Matsuo


The Proceedings of Conference of Kyushu Branch | 2010

502 An Experimental Study on Choking of Duct Flows with Boundary Layers

Kazunori Kubo; Kazuyasu Matsuo


The Proceedings of Conference of Kyushu Branch | 2010

505 Experimental Study on Compressible Choked Flow of Curved Channel

Hideki Yamamoto; Hiroki Yanagi; Tsuyoshi Yasunobu; Yoshiaki Miyazato; Kazuyasu Matsuo


The Proceedings of the Fluids engineering conference | 2009

0606 Sonic Conductance and Total Pressure Loss in Fanno Flows

Hideki Yamamoto; Tsuyoshi Yasunobu; Yoshiaki Miyazato; Kazuyasu Matsuo

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Jin Kawakita

National Institute for Materials Science

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Seiji Kuroda

National Institute for Materials Science

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