CiNii Articles - TAKEISHI Ken-ichiro

1

1. 全般(2011年国際ガスタービン会議大阪大会,創立40周年記念) [in Japanese]

TAKEISHI Kenichiro

Journal of the Gas Turbine Society of Japan 40(2), 114-115, 2012-03-20
2

2011年国際ガスタービン会議大阪大会 [in Japanese]

TAKEISHI Kenichiro , FUJIOKA Terutaka , OKAI Keiichi , HASEGAWA Takeharu , NOZAKI Osamu , WATANABE Toshinori , TSUJIMOTO Yoshinobu , YAMAMOTO Makoto , NAKADA Toshihiko , IMANARI Kuniyuki , MAKINO Atsushi , OHTA Yutaka , SHIBATA Takanori , ITO Eisaku , FUNAZAKI Ken-ichi , AKAMATSU Fumiteru , KANEKO Shigehiko , IKI Norihiko , TANUMA Tadashi , SAITO Eiji , YOSHIOKA Yomei , TAMAKI Hideaki , IBARAKI Seiichi , KODA Eiichi , TANIMURA Kazuhiko , FURUKAWA Hiroyuki , NISHIOKA Takahiro , MASADA Junichiro , KINOSHITA Yasuhiro

日本ガスタービン学会誌 40(2), 114-133, 2012-03-20
3

Heat Transfer [in Japanese]

TAKEISHI Kenichiro , MURATA Akira

Journal of the Gas Turbine Society of Japan 39(5), 360-362, 2011-09-20
4

Heat Transfer [in Japanese]

FUNAZAKI Kenichi , TAKEISHI Kenichiro , ISHIDA Katsuhiko

Journal of the Gas Turbine Society of Japan 38(5), 352-354, 2010-09-20
5

Progress of Cooling Technologies for Gas Turbine Blades and Vanes [in Japanese]

TAKEISHI Kenichiro

Journal of the Gas Turbine Society of Japan 38(2), 78-84, 2010-03-20

References (30) Cited by (2)
6

Study on Heat Transfer and Film Cooling for Next Generation High Temperature Industrial Gas Turbine Blades [in Japanese]

KITAMURA Tsuyoshi , MATSUURA Masaaki , HADA Satoshi , TSUKAGOSHI Keizo , TAKEISHI Ken-ichiro

Heat transfer coefficient and film cooling effectiveness on a rotating turbine blade have been studied by using a Low-Speed Research Turbine (LSRT) facility. The turbine model airfoils applied to LSRT …

Journal of the Gas Turbine Society of Japan 37(6), 392-398, 2009-11-20

References (19)
7

A-15 Study on Film Cooling for a Rotating Turbine Blade Platform [in Japanese]

KITAMURA Tsuyoshi , MATSUURA Masaaki , TORII Shunsuke , TSUKAGOSHI Keizo , TAKEISHI Ken-ichiro

Film cooling effectiveness on a rotating turbine blade platform have been studied by using a Low-Speed Research Turbine (LSRT) facility. The turbine model airfoils applied to LSRT were high loaded typ …

ガスタービン定期講演会講演論文集 (37), 89-94, 2009-10-21
8

Progress of Technologies to Challenge Industrial Gas Turbines [in Japanese]

TAKEISHI Kenichiro

Journal of the Society of Mechanical Engineers 112(1092), 876-879, 2009

J-STAGE References (13) Cited by (2)
9

A-2 Study on Heat Transfer and Film Cooling for Next Generation Gas Turbines [in Japanese]

KITAMURA Tsuyoshi , MATSUURA Masaaki , HADA Satoshi , Tsukagoshi Keizo , Takeishi Ken-ichiro

Heat transfer coefficient and film cooling effectiveness in a rotating blade have been measured with a Low-Speed Research Turbine (LSRT) facility. The turbine model airfoils applied to LSRT were high …

ガスタービン定期講演会講演論文集 (36), 25-30, 2008-10-01
10

Development of High Performance Film Cooling of 1700 Degree C Class Gas Turbines [in Japanese]

HADA Satoshi , MATSUURA Masaaki , TSUKAGOSHI Keizo , TAKEISHI Kenichiro

Journal of High Temperature Society 33(5), 264-272, 2007-09-26

References (14) Cited by (1)
11

Technology Development of an Advanced 1700℃-class Heavy Duty Gas Turbine [in Japanese]

ITO Eisaku , TSUKAGOSHI Keizo , TAKEISHI Kenichiro

Journal of High Temperature Society 33(5), 222-228, 2007-09-26

J-STAGE References (6) Cited by (1)
12

Overview [in Japanese]

TAKEISHI Kenichiro

Journal of the Gas Turbine Society of Japan 35(5), 355-356, 2007-09-20
13

Current and Future Status on Large LNG Burning Combined Power Plants [in Japanese]

TAKEISHI Kenichiro

Large LNG burning gas-steam combined cycle power plants whose thermal efficiencies are about 30% higher than that of coal burning thermal power plants have been high-lighted against global warming as …

Journal of the Japan Institute of Energy 86(7), 436-442, 2007-07-20

References (13) Cited by (1)
14

Progress of Film Cooling Technologies [in Japanese]

TAKEISHI Kenichiro

Journal of the Gas Turbine Society of Japan 35(3), 156-164, 2007-05-20

References (84)
15

3rd International Conference on the Future of Gas Turbine Technology [in Japanese]

TAKEISHI Ken ichiro

Journal of the Gas Turbine Society of Japan 35(1), 37-39, 2007-01-20
16

F02(1) Advanced Cooling Technologies of Turbine Blades and Vanes for 1700℃ Class Gas Turbines [in Japanese]

TAKEISHI Kenichiro , ITO Eisaku

The Reference Collection of Annual Meeting 2007.8(0), 159-160, 2007

J-STAGE
17

0410 Study on Heat Transfer Characteristics of a Circular Air Jet Impingement in Closed Cavities [in Japanese]

TAKEISHI Kenichiro , ITO Ryuta , TSUKAGOSHI Keizo , MATSUURA Masaaki , KITAMURA Tsuyoshi , Ito Eisaku

One of the new cooling concepts of turbine nozzle and blade endwall for next generation 1700℃ class industrial gas turbines is an impingement cooling technology in a closed cavity. As the turbine inle …

The proceedings of the JSME annual meeting 2007.3(0), 5-6, 2007

J-STAGE
18

A Study on Retardation of Laminar Flame Extinction due to Locally Controlled Stretch Rate [in Japanese]

MATSUMURA Yoshikazu , TAKAGI Toshimi , KINOSHITA Shinichi , TAKEISHI Ken-ichiro

Turbulent diffusion flame is supposed to be composed of a lot of laminar diffusion flamelets. To understand extinction processes of the flamelet, counterflow diffusion flame has been used. It was well …

Transactions of the Japan Society of Mechanical Engineers B 72(715), 790-796, 2006-03-25

References (15) Cited by (1)
19

For the Special Issue on Medium and Small Gas Turbines [in Japanese]

TAKEISHI Kenichiro

Journal of the Gas Turbine Society of Japan 34(1), 1-2, 2006-01-20

References (4)
20

ガスタービンにおける熱流動計測技術 (特集:最近のターボ機械流れ計測技術) [in Japanese]

武石賢一郎 , 川田裕

Turbomachinery. 33(11), 688-695, 2005-11

武石賢一郎 TAKEISHI Ken-ichiro

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武石 賢一郎 TAKEISHI Ken-ichiro

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武石賢一郎 TAKEISHI Ken-ichiro

Articles:　 1-20 of 22