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Proceedings Papers

Calculation of Transitional Boundary Layers With an Improved Low-Reynolds Number Version of the k-ε Turbulence Model

Proc. ASME. GT1993, Volume 2: Combustion and Fuels; Oil and Gas Applications; Cycle Innovations; Heat Transfer; Electric Power; Industrial and Cogeneration; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; IGTI Scholar Award, V002T08A005, May 24–27, 1993

Paper No: 93-GT-073

DOI: https://doi.org/10.1115/93-GT-073

View Paper titled, Calculation of Transitional Boundary Layers With an Improved Low-Reynolds Number Version of the k-ε Turbulence Model

Topics: Boundary layers, Turbulence, Damping, Flow (Dynamics), Heat transfer, Reynolds number, Blades, Gas turbines, Modeling, Pressure gradient

Proceedings Papers

Prediction of Vane Surface Film Cooling Effectiveness Using Compressible Navier-Stokes Procedure and k-ε Turbulence Model With Wall Function

Yoshitaka Fukuyama, Fumio Otomo, Minoru Sato, Yuichi Kobayashi, Hiroyuki Matsuzaki

Proc. ASME. GT1995, Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, V004T09A025, June 5–8, 1995

Paper No: 95-GT-025

DOI: https://doi.org/10.1115/95-GT-025

View Paper titled, Prediction of Vane Surface Film Cooling Effectiveness Using Compressible Navier-Stokes Procedure and k-ε Turbulence Model With Wall Function

Topics: Cooling, Thin films, Turbulence, Film cooling, Geometry, Pressure, Turbines, Convection, Reynolds number, Winding (process)

Proceedings Papers

Aerodynamic Loss Increase due to Individual Film Cooling Injections From Gas Turbine Nozzle Surface

Ryo Kubo, Fumio Otomo, Yoshitaka Fukuyama, Yuhji Nakata

Proc. ASME. GT1998, Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, V004T09A083, June 2–5, 1998

Paper No: 98-GT-497

DOI: https://doi.org/10.1115/98-GT-497

View Paper titled, Aerodynamic Loss Increase due to Individual Film Cooling Injections From Gas Turbine Nozzle Surface

Topics: Film cooling, Gas turbines, Nozzles, Pressure, Flow (Dynamics), Design, Cascades (Fluid dynamics), Computation, Computational fluid dynamics, Modeling

Proceedings Papers

Design Study of Helium Turbine for the 300MW HTGR-GT Power Plant

Yasushi Muto, Shintaro Ishiyama, Yoshitaka Fukuyama, Junji Okumoto, Tadaharu Kishibe, Seiya Yamada

Proc. ASME. GT2000, Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations, V002T04A010, May 8–11, 2000

Paper No: 2000-GT-0159

DOI: https://doi.org/10.1115/2000-GT-0159

View Paper titled, Design Study of Helium Turbine for the 300MW HTGR-GT Power Plant

Topics: Design, Helium, Power stations, Turbines, Very high temperature reactors, Compressors, Cycles, Generators, Pressure, Rotordynamics

Proceedings Papers

Experimental Study on Racetrack-Shaped Holes Impingement Cooling With Bump Type Roughening Element

Chiyuki Nakamata, Yoji Okita, Takashi Yamane, Yoshitaka Fukuyama, Toyoaki Yoshida

Proc. ASME. GT2012, Volume 4: Heat Transfer, Parts A and B, 425-434, June 11–15, 2012

Paper No: GT2012-69077

DOI: https://doi.org/10.1115/GT2012-69077

View Paper titled, Experimental Study on Racetrack-Shaped Holes Impingement Cooling With Bump Type Roughening Element

Topics: Impingement cooling, Cooling, Reynolds number, Flow (Dynamics)

Journal Articles

Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Shu Fujimoto, Yoji Okita, Yoshitaka Fukuyama, Takashi Yamane, Fujio Mimura, Masahiro Matsushita, Toyoaki Yoshida

J. Turbomach. July 2010, 132(3): 031019.

DOI: https://doi.org/10.1115/1.3151602

Published Online: April 7, 2010

View Article titled, Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Topics: Cooling

Proceedings Papers

Leading Edge Cooling Performance of an Integrated Cooling Configuration

Takahiro Bamba, Takao Kumagai, Fujio Mimura, Takashi Yamane, Yoshitaka Fukuyama, Taiki Usui, Toyoaki Yoshida

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 553-561, June 9–13, 2008

Paper No: GT2008-50574

DOI: https://doi.org/10.1115/GT2008-50574

View Paper titled, Leading Edge Cooling Performance of an Integrated Cooling Configuration

Topics: Cooling

Proceedings Papers

Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Shu Fujimoto, Yoji Okita, Yoshitaka Fukuyama, Takashi Yamane, Fujio Mimura, Masahiro Matsushita, Toyoaki Yoshida

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 431-441, June 9–13, 2008

Paper No: GT2008-50444

DOI: https://doi.org/10.1115/GT2008-50444

View Paper titled, Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Topics: Aircraft engines, Cooling, Nozzles, Pressure, Turbines, Airfoils, Reynolds number, Air flow, Blades, Design

Proceedings Papers

Turbulence Model Dependencies on Conjugate Simulation of Flow and Heat Conduction

Takahiro Bamba, Takashi Yamane, Yoshitaka Fukuyama

Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 635-643, May 14–17, 2007

Paper No: GT2007-27824

DOI: https://doi.org/10.1115/GT2007-27824

View Paper titled, Turbulence Model Dependencies on Conjugate Simulation of Flow and Heat Conduction

Topics: Flow (Dynamics), Heat conduction, Heat transfer, Simulation, Turbulence

Proceedings Papers

Local Cooling Effectiveness Distribution of an Integrated Impingement and Pin Fin Cooling Configuration

Chiyuki Nakamata, Fujio Mimura, Masahiro Matsushita, Takashi Yamane, Yoshitaka Fukuyama, Toyoaki Yoshida

Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 23-34, May 14–17, 2007

Paper No: GT2007-27020

DOI: https://doi.org/10.1115/GT2007-27020

View Paper titled, Local Cooling Effectiveness Distribution of an Integrated Impingement and Pin Fin Cooling Configuration

Topics: Cooling

Proceedings Papers

Conceptual Design and Cooling Blade Development of 1700 °C-Class High-Temperature Gas Turbine

Shoko Ito, Hiroshi Saeki, Asako Inomata, Fumio Ootomo, Katsuya Yamashita, Yoshitaka Fukuyama, Eiichi Koda, Toru Takahashi, Mikio Sato, Miki Koyama, Toru Ninomiya

Proc. ASME. GT2003, Volume 1: Turbo Expo 2003, 829-842, June 16–19, 2003

Paper No: GT2003-38352

DOI: https://doi.org/10.1115/GT2003-38352

View Paper titled, Conceptual Design and Cooling Blade Development of 1700 °C-Class High-Temperature Gas Turbine

Topics: Blades, Conceptual design, Cooling, Gas turbines, High temperature, Heat transfer, Steam, Thermal efficiency, Carbon dioxide, Closed-cycle gas turbines

Proceedings Papers

Spatial Arrangement Dependance of Cooling Performance of an Integrated Impingement and Pin Fin Cooling Configuration

Chiyuki Nakamata, Yoji Okita, Shinsuke Matsuno, Fujio Mimura, Masahiro Matsushita, Takashi Yamane, Yoshitaka Fukuyama, Toyoaki Yoshida

Proc. ASME. GT2005, Volume 3: Turbo Expo 2005, Parts A and B, 385-395, June 6–9, 2005

Paper No: GT2005-68348

DOI: https://doi.org/10.1115/GT2005-68348

View Paper titled, Spatial Arrangement Dependance of Cooling Performance of an Integrated Impingement and Pin Fin Cooling Configuration

Topics: Computational fluid dynamics, Cooling, Film cooling, Heat transfer, Density, Reynolds number, Temperature, Flow (Dynamics), Gas flow, Impingement cooling

Journal Articles

Conceptual Design and Cooling Blade Development of 1700°C Class High-Temperature Gas Turbine

Shoko Ito, Hiroshi Saeki, Asako Inomata, Fumio Ootomo, Katsuya Yamashita, Yoshitaka Fukuyama, Elichi Koda, Toru Takehashi, Mikio Sato, Miki Koyama, Toru Ninomiya

J. Eng. Gas Turbines Power. April 2005, 127(2): 358–368.

DOI: https://doi.org/10.1115/1.1806456

Published Online: April 15, 2005

View Article titled, Conceptual Design and Cooling Blade Development of 1700°C Class High-Temperature Gas Turbine

Topics: Blades, Cooling, Nozzles, High temperature, Heat transfer, Flow (Dynamics), Gas turbines, Turbines, Coolants, Rotors

Journal citation

NARROW

Calculation of Transitional Boundary Layers With an Improved Low-Reynolds Number Version of the k-ε Turbulence Model

Prediction of Vane Surface Film Cooling Effectiveness Using Compressible Navier-Stokes Procedure and k-ε Turbulence Model With Wall Function

Aerodynamic Loss Increase due to Individual Film Cooling Injections From Gas Turbine Nozzle Surface

Design Study of Helium Turbine for the 300MW HTGR-GT Power Plant

Experimental Study on Racetrack-Shaped Holes Impingement Cooling With Bump Type Roughening Element

Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Leading Edge Cooling Performance of an Integrated Cooling Configuration

Study on Advanced Internal Cooling Technologies for the Development of Next-Generation Small-Class Aircraft Engines

Turbulence Model Dependencies on Conjugate Simulation of Flow and Heat Conduction

Local Cooling Effectiveness Distribution of an Integrated Impingement and Pin Fin Cooling Configuration

Conceptual Design and Cooling Blade Development of 1700 °C-Class High-Temperature Gas Turbine

Spatial Arrangement Dependance of Cooling Performance of an Integrated Impingement and Pin Fin Cooling Configuration

Conceptual Design and Cooling Blade Development of 1700°C Class High-Temperature Gas Turbine

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