International Gas Turbine Congress 2019 Tokyo
November 17-22, 2019, Tokyo, Japan

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Last updated on October 29, 2019. This conference program is tentative and subject to change

Technical Program for Tuesday November 19, 2019

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TuAM11 Room A
aFJR Technical Session
 
09:00-09:25, Paper TuAM11.1 
Development of Hollow Composite Fan Blade
Kuroki, HiroshiIHI Corporation
Hosaka, ToshihikoIHI Corporation
Takeda, TomoJapan Aerospace Exploration Agency
Hojo, MasahiroJapan Aerospace Exploration Agency
Nishizawa, ToshioJapan Aerospace Exploration Agency
Yoshikawa, NobuhiroThe University of Tokyo
 
09:25-09:50, Paper TuAM11.2 
Experimental Study of Laminar Flow Effect for Transonic Engine Fan
Hayashi, RyosukeIHI Corporation
Nozomi, TanakaIHI Corporation
Enoki, TomonoriIHI Corporation
Murooka, TakeshiIHI
Kato, DaiIHI Corporation
Masaki, DaisakuJAXA
Kazawa, JunichiJAXA
Enomoto, ShunjiJAXA
Nishizawa, ToshioJapan Aerospace Exploration Agency
 
09:50-10:15, Paper TuAM11.3 
Detection of Cascade Flutter in a Low-Pressure Turbine
Hachijo, TakayoshiTokyo University of Science
Kobayashi, HiroakiTokyo University of Science
Hayashi, YutoTokyo University of Science
Gotoda, HiroshiTokyo University of Science
Nishizawa, ToshioJapan Aerospace Exploration Agency
Kazawa, JunichiJAXA
 
10:15-10:40, Paper TuAM11.4 
Development of Resin-Based Lightweight Acoustic Liner
Kagaya, RyoIHI Corporation
Sakamoto, MaiIHI Corporation
Oishi, TsutomuIHI
Ishii, TatsuyaJAXA
Hojo, MasahiroJapan Aerospace Exploration Agency
Nishizawa, ToshioJapan Aerospace Exploration Agency
 
10:40-11:05, Paper TuAM11.5 
Effect on Acoustic Absorption Properties of Flow Condition and Mach Number in the Grazing Flow
Morita, HitoshiKanazawa Institute of Technology
Akamisaka, YusukeKanazawa Institute of Technology
Toh, HidemiKanazawa Institute of Technology
Enomoto, ShunjiJAXA
Ishii, TatsuyaJAXA
Nagai, KenichiroJAXA
 
TuAM12 Room B
Film Cooling Technical Session
 
09:00-09:25, Paper TuAM12.1 
A 3D Conjugate Method to Analyze Turbine Vane with Film Cooling
Wang, LangTsinghua University
Shi, WeiTsinghua
Li, XueyingTSINGHUA UNIVERSITY
Ren, JingTSINGHUA UNIVERSITY
Jiang, HongdeTSINGHUA UNIVERSITY
 
09:25-09:50, Paper TuAM12.2 
Visualization of Film Cooling Flow in Enlarged Model with Particle Image Velocimetry
Asaumi, NorioIHI
Ideta, TakeomiIHI Corporation
Tanaka, YuhiIHI
Matsuno, ShinsukeIHI Corporation
Kubo, SeijiIHI Corporation
 
09:50-10:15, Paper TuAM12.3 
Effects of Oscillations in the Main Flow on Film Cooling for Triple Holes
Baek, Seung IlKookmin University
Ahn, JoonKookmin University
 
10:15-10:40, Paper TuAM12.4 
Unsteady Analysis of the Effects of Density Ratio on Film Cooling Measured by Using PC-PSP
Tanaka, YudaiKansai University
Oda, YutakaKansai University
Takeishi, KenichiroTokushima Bunri University
 
10:40-11:05, Paper TuAM12.5 
Title: Comparison between RANS and Large Eddy Simulations for Nekomimi and 777-Shaped Film Cooling Holes
Dickhoff, JensB&B-AGEMA GmbH
Schneider, MichaelB&B-AGEMA
Kusterer, KarstenB&B-AGEMA GmbH
Bohn, DieterRWTH Aachen University
Horiuchi, TakeshiKawasaki Heavy Industries, Ltd
Fukuda, MeiKawasaki Heavy Industries, LTD
 
TuAM14 Room D
Structural Vibration & Damping Technical Session
 
09:00-09:25, Paper TuAM14.1 
Study on Vibration Response Characteristics of Turbine Blade for Turbocharger
Kaneko, YasutomoRyukoku University
Mori, KazushiMitsubishi Heavy Industries, Ltd
Ebisu, MotokiMitsubishi Engine & Turbocharger Ltd
Ogawa, ShinjiMitsubishi Heavy Industries, Ltd
Takeshita, TomoakiMitsubishi Heavy Industries, Ltd
 
09:25-09:50, Paper TuAM14.2 
Experimental Study on Blade Vibration of Double-Scroll Turbine
Murae, ShotaIHI Corporation
Sato, WataruIHI Corporation
Yamagata, AkihiroIHI Corporation
 
09:50-10:15, Paper TuAM14.3 
Experimental Validation of Transient Resonance Passages of Mistuned Cyclic Structures
Schlesier, Klaus-DieterLeibniz Universität Hannover
Panning-von Scheidt, LarsInstitute for Dynamics and Vibration Research, Leibniz Universit
Wallaschek, JörgInstitute for Dynamics and Vibration Research, Leibniz Universit
 
10:15-10:40, Paper TuAM14.4 
Coupled Wear-Vibration Evolution of Bladed Disks with Friction Contact Interfaces
Heinze, TorstenLeibniz University Hannover
Panning-von Scheidt, LarsInstitute for Dynamics and Vibration Research, Leibniz Universit
Wallaschek, JörgInstitute for Dynamics and Vibration Research, Leibniz Universit
Hartung, AndreasMTU Aero Engines AG
 
10:40-11:05, Paper TuAM14.5 
Probabilistic Study of Blend Repairs on an Axial Compressor Blisk Using the Subset of Nominal Modes Method
Schwerdt, LukasLeibniz Universität Hannover
Berger, RicardaLeibniz Universität Hannover, Institute of Structural Analysis
Panning-von Scheidt, LarsInstitute for Dynamics and Vibration Research, Leibniz Universit
Gebhardt, Cristian GuillermoLeibniz Universität Hannover, Institute of Structural Analysis
Wallaschek, JörgInstitute for Dynamics and Vibration Research, Leibniz Universit
Rolfes, RaimundLeibniz Universität Hannover, Institute of Structural Analysis
 
TuAM15 Room E
Combustion CFD Technical Session
 
09:00-09:25, Paper TuAM15.1 
Validity of Non-Adiabatic FGM Approach for Numerical Simulation of Flame Propagation in the Vicinity of the Wall
Kai, ReoKyoto University
Takenaka, KenichiroKyoto University
Kurose, RyoichiKyoto University
 
09:25-09:50, Paper TuAM15.2 
Numerical Simulation of CO Concentration on Flame Propagation in the Vicinity of the Wall
Yunoki, KeitaMitsubishi Heavy Industries
Kai, ReoKyoto University
Inoue, ShinpeiKyoto University
Konishi, KentoKyoto University
Kurose, RyoichiKyoto University
 
09:50-10:15, Paper TuAM15.3 
Numerical Simulations of the Micromix DLN Hydrogen Combustion Technology with LES and Comparison to Results of RANS and Experimental Data
Striegan, Constantin J. D.B&B-AGEMA GmbH
Struth, BenjaminRWTH Aachen University
Dickhoff, JensB&B-AGEMA GmbH
Kusterer, KarstenB&B-AGEMA GmbH
Funke, Harald H.-W.Aachen Univeristy of Applied Sciences
Bohn, DieterRWTH Aachen University
 
10:15-10:40, Paper TuAM15.4 
Numerical Study of the Parially Premixed Swirl Flame Dynamics Using POD/DMD Method
Yang, YangInstitute of Engineering Thermophysics, Chinese Academy of Scien
 
10:40-11:05, Paper TuAM15.5 
A Study on Efficient Calculation of Mixture Transport Properties by Artificial Neural Network
Yamamoto, HimekoWaseda University
Mizobuchi, YasuhiroJapan Aerospace Exploration Agency
Sato, TetsuyaWaseda University
 
TuAM16 Room F
Aerodynamic and Design of Gas Turbines: Multi-Physics-1 Technical Session
 
09:00-09:25, Paper TuAM16.1 
Uncertainty Quantification of the Aerodynamic Performance of Supercritical Carbon Dioxide Compressor
Ma, CanScience and Technology on Thermal Energy and Power Laboratory
Lin, YuanshengScience and Technology on Thermal Energy and Power Laboratory
Gou, JinlanWuhan Second Ship Design and Research Institute
Wang, WeiScience and Technology on Thermal Energy and Power Laboratory
Lyu, WeijianScience and Technology on Thermal Energy and Power Laboratory
 
09:25-09:50, Paper TuAM16.2 
Numerical Investigation on Property Effects in a Low Speed Axial Supercritical Carbon Dioxide Compressor
Gou, JinlanWuhan Second Ship Design and Research Institute
Wang, WeiScience and Technology on Thermal Energy and Power Laboratory
Ma, CanWuhan Second Ship Design and Research Institute
Chonghai, HuangWuhan Second Ship Design and Research Institute
Huafeng, LiWuhan Second Ship Design and Research Institute
Yang, LinpingChongqing Huayu Electric Group Co. Ltd
 
09:50-10:15, Paper TuAM16.3 
Numerical Investigation of Supercritical CO2 Flows in a Radial Compressor with Real Gas Model
Furusawa, TakashiTohoku University
Hao, JianmingTohoku University
Moriguchi, ShotaTohoku Univesity
Miyazawa, HironoriTohoku University
Yamamoto, SatoruTohoku University
 
10:15-10:40, Paper TuAM16.4 
Computational Study of Deposition Phenomena on High-Pressure Turbine Vane Using UPACS
Mizutori, KentaTokyo University of Science
Fukudome, KojiTokyo University of Science
Yamamoto, MakotoTokyo University of Science
Suzuki, MasayaJapan Aerospace Exploration Agency
 
TuIL1PL Room A
Plenary Session-2 Plenary Session
 
11:25-12:25, Paper TuIL1PL.1 
Key Combustion Challenges for Future Gas Turbines
Lieuwen, TimothyGeorgia Institute of Technology
 
TuIL2PL Room A
Plenary Session-3 Plenary Session
 
14:00-15:00, Paper TuIL2PL.1 
Improving Aerothermal and Aeromechanical Turbomachinery Design by Combining High-Fidelity Methods with Multi-Stage Approaches
Seume, Joerg R.Leibniz University Hannover
 
TuPM11 Room A
Propulsion-Aircraft Integration & Electrification Technical Session
 
15:20-15:45, Paper TuPM11.1 
Unsteady Flow in a Short Highly Bent Intake Duct
Haug, Jakob PhilippBundeswehr University Munich
Rademakers, Rudolf P.M.Institute of Jet Propulsion, Bundeswehr University Munich
Krummenauer, MichaelWehrtechnische Dienststelle Für Luftfahrzeuge Und Luftfahrtgerät
Niehuis, ReinhardUniversity of the German Federal Armed Forces Munich
 
15:45-16:10, Paper TuPM11.2 
Experimental Investigation of a Novel Boundary Layer Ingestion Engine Intake with S-Shaped Geometry
Gaitanis, Aggelos EvripidisAristotle University of Thessaloniki
Efstathiadis, TheofilosAristotle University of Thessaloniki
Kalfas, AnestisAristotle University of Thessaloniki
 
16:10-16:35, Paper TuPM11.3 
Experimental Investigation on the Effect of Boundary Layer Ingestion Using a Two-Dimensional Airfoil
Tsuruta, RyosukeWaseda University
Mitani, YoshihiroWaseda University
Ogushi, ShotaroWaseda University
Okuno, AkikoWaseda University
Sato, TetsuyaWaseda University
Harada, MasashiJapan Aerospace Exploration Agency
Okai, KeiichiJapan Aerospace Exploration Agency
 
16:35-17:00, Paper TuPM11.4 
Feasibility Study on Turboelectric System Based on Engine-Cycle Analysis and Fuel Consumption of Commercial Aircraft
Iwasaki, YusukeThe University of Tokyo
Watanabe, ToshinoriThe University of Tokyo
Himeno, TakehiroThe University of Tokyo
Tateishi, AtsushiThe University of Tokyo
Sakuma, YasunoriThe University of Tokyo
 
TuPM12 Room B
Novel Cooling Technologies Technical Session
 
15:20-15:45, Paper TuPM12.1 
Flow and Heat Transfer Characteristics in a Double-Wall Cooling System with a Hexagonal Film Hole Arrangement
Liu, YuyangShanghai Jiao Tong University
Rao, YuShanghai Jiao Tong University
Yang, LiShanghai Jiao Tong University
 
15:45-16:10, Paper TuPM12.2 
Studies on the Effect of Vortex Generators on Film Cooling Effectiveness Based on a High-Order LES Turbulence Model
Biswas, DebasishToshiba Corporation
 
16:10-16:35, Paper TuPM12.3 
Study on Thermofluid Characteristics of a Lattice Cooling Channel
Tsuru, TomokoKawasaki Heavy Industries, Ltd
Morozumi, RyoTokushima Bunri University
Takeishi, KenichiroTokushima Bunri University
 
16:35-17:00, Paper TuPM12.4 
Thermodynamic Stability Condition of Swirling Flows in Convergent Vortex Tubes
Seibold, FlorianUniversity of Stuttgart, Institute of Aerospace Thermodynamics
Weigand, BernhardUniversity of Stuttgart
Marsik, FrantisekWest Bohemia University Plzen
Novotny, PavelInstitute of Aerospace Thermodynamics, University of Stuttgart,
 
TuPM13 Room C
Compressor Technical Session
 
15:20-15:45, Paper TuPM13.1 
Influence of Inlet Geometry on the Performance of High Pressure Ratio Centrifugal Compressor
Yang, HaosenHelan Turbines Co., Ltd
Zheng, TianHuaHelan Turbines Co., Ltd
Gao, ChuangShanghai Advanced Research Institute, Chinese Academy of Science
 
15:45-16:10, Paper TuPM13.2 
Operating Range Enhancement by Tip Leakage Vortex Breakdown Control of a Centrifugal Compressor
Tomita, IsaoMitsubishi Heavy Industries, Ltd
Furukawa, MasatoKyushu University
 
16:10-16:35, Paper TuPM13.3 
Prediction of Turbocharger Compressor Surge on Engine
Tokieda, KatsunoriIHI Corporation
Bamba, TakahiroIHI Corporation
Fujiwara, TakashiIHI Corporation
Kakudate, YukiyaIHI Corporation
 
16:35-17:00, Paper TuPM13.4 
Study on Blade Vibration of Centrifugal Compressor -Reduction of Vibratory Stress by Asymmetric Vaned Diffuser -
Shimohara, NaotoIHI Corporation
Mikami, ChihiroIHI Corporation
Hattori, HiroakiIHI Corporation
 
TuPM14 Room D
Unsteady Flow and Flow Control-2 Technical Session
 
15:20-15:45, Paper TuPM14.1 
Unsteady Flow Phenomena in a Shrouded Four Stage Axial Air Turbine
Winhart, BenjaminRuhr-Universität Bochum
von Gosen, FlorianRuhr-Universität Bochum
di Mare, FrancescaRuhr-Universität Bochum
 
15:45-16:10, Paper TuPM14.2 
Stabilization of a Two-Stage Axial Compressor with Stall Precursor-Suppressed (SPS) Casing Treatment
Dong, XuBeihang University
Sun, DakunBeihang University
Hu, GuotunChina Academy of Launch Vehicle Technology
Sun, XiaofengBeiHang University
 
16:10-16:35, Paper TuPM14.3 
Stability Improvement of Circumferential Grooves on a Low Speed Axial Compressor under Inlet Radial Total Pressure Distortion Conditions
Li, YihanInstitute of Engineering Thermophysics, Chinese Academy of Scien
Du, JuanChinese Academy of Sciences
Zhang, QianfengInstitute of Engineering Thermophysics, Chinese Academy of Scien
Li, ZhihuiChinese Academy of Sciences
Li, Ji-ChaoChinese Academy of Science
Zhang, HongwuInstitute of Engineering Thermophysics, Chinese Academy of Scien
 
TuPM15 Room E
Fuel and Flame Diagnostic Technical Session
 
15:20-15:45, Paper TuPM15.1 
Spray Flux Distribution of High-Speed Planar Air-Blast Atomizer
Yoshida, HiroakiKyushu University
Inoue, ChihiroKyushu University
Kouwa, JunyaIHI Corporation
Itoh, MitsunoriIHI Corporation
 
15:45-16:10, Paper TuPM15.2 
Flame Diagnostics Method for Oil Fired Industrial Gas Turbine Combustors under High Pressure Conditions
Miyazaki, KojiMitsubishi Heavy Industries, Ltd
Noda, JunjiMitsubishi Heavy Industries, Ltd
Kimura, YuichiroMitsubishi Heavy Industries, LTD
Saitoh, ToshihikoMitsubishi Heavy Industries, LTD
 
16:10-16:35, Paper TuPM15.3 
Combustion of CH4/H2 Mixtures in Gas Turbines - Flame Speed and Risk of Flashback
Jansohn, PeterPaul Scherrer Institute (PSI)
Ebi, DominikPaul Scherrer Institute (PSI)
 
16:35-17:00, Paper TuPM15.4 
Nonlinear Dynamics of Oxy-Fuel Combustion in a Laboratory-Scale Gas-Turbine Model Combustor
Takeda, NaohiroTokyo University of Science
Kinoshita, SatoshiRitsumeikan University
Murayama, ShogoTokyo University of Science
Gotoda, HiroshiTokyo University of Science
 
TuPM16 Room F
Aerodynamic and Design of Axial Compressors-3 Technical Session
 
15:20-15:45, Paper TuPM16.1 
Development and Verification of Automated Design System for Transonic Compressor Airfoil
Niwa, NaoyukiKawasaki Heavy Industries, Ltd
Kanazawa, NaokiKawasaki Heavy Industries
Sakai, YusukeKawasaki Heavy Industries
Matsuoka, AkinoriKawasaki Heavy Industries, LTD
 
15:45-16:10, Paper TuPM16.2 
Performance Analysis of a Compressor Leading Edge without Pressure Spike at High Subsonic Speed
Lang, HenningRWTH Aachen University
Goto, TakashiIHI Corporation
Sato, DaisukeIHI Corporation
Kato, DaiIHI Corporation
Jeschke, PeterRWTH Aachen University
 
16:10-16:35, Paper TuPM16.3 
Experimental Investigation of the Flow Characteristics in a Circumferential Bleed Port Geometry and the Interaction with a 1.5-Stage Axial Compressor
Achmus, MelanieTechnical University Braunschweig
Friedrichs, JensTU Braunschweig, Institute for Jet Propulsion and Turbomachinery
Becker, BerndRolls-Royce Deutschland Ltd. & Co. KG

 
 

 
 

 

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