Preliminarily distributed documents

ASIAN CONGRESS ON GAS TURBINES 2012 (ACGT2012)━ Tradition, Challenge and Future

Shanghai, P. R. China
August 20-22, 2012

Organized by

Institute of Engineering Thermophysics, Chinese Academy of Sciences
Gas Turbine Society of Japan
Korean Fluid Machinery Association

ASIAN CONGRESS ON GAS TURBINES 2012

Contents

Organization of Asian Congress on Gas Turbines 2012 ......................1
Message from the Organizing Committee ............................................3
About Asian Congress on Gas Turbines 2012......................................4
Location of Congress and Banquet Venue ...........................................5
Shuttle Bus Drive Route and Departure Time ......................................9
Plant Tour............................................................................................10
Schedule at a Glance ...........................................................................12
Program Overview ..............................................................................13
Keynote and Forum Session ...............................................................14
Session Program .................................................................................15
General Information ............................................................................20

Organization of Asian Congress on Gas Turbines 2012Organizing Society

Institute of Engineering Thermophysics, Chinese Academy of Sciences (IET/CAS)
Gas Turbine Society of Japan (GTSJ)
Korean Fluid Machinery Association (KFMA)

Organizing Committee

Osamu Kawaguchi(Keio University, Japan)

Toshinori Watanabe(University of Tokyo, Japan)

Makoto Yamamoto(Tokyo University of Science, Japan)

Soo-Seok Yang

(Korea Aerospace Research Institute, Korea)

Daesung Lee(Korea Aerospace Research Institute, Korea)

Seung Jin Song

(Seoul National University, Korea)

Chen Jingyi(Institute of Engineering Thermophysics / Chinese Academyof Sciences, China)

Sun Xiaofeng(Beijing University of Aeronautics and Astronautics, China)

Huang Weiguang(Shanghai Advanced Research Institute / Chinese Academyof Sciences, China)Local Organizing Committee

Weng Shilie(Shanghai Jiaotong University)

Su Ming(Shanghai Jiaotong University)

Zang Shusheng(Shanghai Jiaotong University)

Yuan Xin(Tsinghua University)

Gui Xingmin(Beihang University)

Feng Zhenping(Xi’an Jiaotong University)

Wang Songtao(Harbin Institute of Technology)

Huang Ou

(Shanghai Electric Group Co., LTD.)

Wang Weimin(Dongfang Electric Corporation Limited)

1(Chairman)

Yao Hongwei(Harbin Turbine Co., LTD.)Li Xiaotang(Aviation Industry Corporation of China)

Lin Feng(China Shipbuilding Industry Corporation)

Zhu Junqiang(Institute of Engineering Thermophysics / Chinese Academy of
Sciences)

Lin Feng(Institute of Engineering Thermophysics / Chinese Academy of
Sciences)

Zhang Hongwu(Institute of Engineering Thermophysics / Chinese Academy of
Sciences)Local Organizers

Shanghai Jiao Tong University (SJTU)
Shanghai Electric Group Company Limited (SEC)
Shanghai Advanced Research Institute / Chinese Academy of Sciences (SARI/CAS)

2

Message from the Organizing Committee
On behalf of the Organizing Committee, I would like to extend my warm
welcome to you all to the Asian Congress on Gas Turbines ACGT 2012
in Shanghai China from August 20th to 22nd 2012.
The ACGT is an international congress on gas turbines started in 2005
and the ACGT2012 is the third one jointly organized by the Institute ofEngineering Thermophysics, Chinese Academy of Sciences (IET/CAS),
the Gas Turbine Society of Japan (GTSJ) and the Korean Fluid
Machinery Association (KFMA). Following the tradition set at the firstand second ACGT conferences held in Korea 2005 and in Japan 2009,
the ACGT2012 will once again aim to provide an international platform
for extensive exchange of information among gas turbine researchers,
users and manufacturers within and outside Asian region.
The ACGT2012 program consists of a keynote lecture by Dr. Aoki Sunao, three keynote speeches
by experts from China, Korea and Japan, a forum session and a plant tour. A total of 100 papers
will be presented during the general sessions, and gas turbine related technologies will also be
exhibited at the congress site. Through the enhancement of interaction and cooperation among
researchers and students, the ACGT2012 is expected to promote Pan-Asian cooperative effort ingas turbine research and development.
Thanks to the dedication and cooperation of many individuals and organizations, including
members of the Organizing Committee and Local Organizing Committee, session chairs andauthors, exhibitors and all participants, who make this congress possible and successful. I hereby
extend my gratitude and appreciation to all of the above-mentioned organizations and individuals
for their contribution and efforts.
Shanghai, as a world-wide known dynamic city, has made great progress in many technologies
including Gas Turbines. I am honoured and delighted to host all of you, my distinguished guests,
and wish Shanghai become a new international platform for researchers and engineers to exchange
their ideas in Gas Turbine technology.
Once again, thank you for attending the ACGT2012, we wish you will enjoy the congress.
Look forward to seeing you all in Shanghai.

Weng Shilie
Chairman
Organizing Committee of the ACGT2012

3

About Asian Congress on Gas Turbines 2012
 Term of Session
August 20(Mon.)-August 22(Wed.)

Congress Venue

Shanghai Jiao Tong University, Minhang Branch Campus
800 Dongchuan Road, Minhang District, Shanghai 200240, China
Objectives

Following the tradition set at the first and second ACGT conferences held in Korea 2005 andJapan 2009, the ACGT2012 will once again aim to provide an international forum forexchange of information related to gas turbine technology, especially among researchers in
Asian Region. Through the enhancement of interaction and cooperation among Asian
researchers and students, the ACGT2012 is expected to promote Pan-Asian cooperative
effort in gas turbine research and development. The ACGT2012 will also act as a platform topromote interactions for gas turbine researchers, users and manufacturers within andoutside Asian region.
Keynote Lecture

Title: To be determined
Lecturer: Prof. Sunao Aoki (Chief Research Fellow, Mitsubishi Research Institute, Inc., and Special adviser to
Mitsubishi Heavy Industries, Ltd.)

Keynote Speech

Speech 1—Title: To be determined
Speaker: Prof. Yasukata Tsutsui (the Ex-President of GTSJ)

Speech 2—Title: To be determined
Speaker: Prof. LI Ye (Director-General, Department of Energy Conservation and Scientific Equipment, National
Energy Administration)

Speech 3—Title: “Optimization of a Novel Film-Cooling Hole for Turbine Blade Cooling”
Speaker: Prof. Kwang-Yong Kim (Inha Fellow Professor, School of Mechanical Engineering, Inha University)



Forum

Topic -- The Trends of Gas Turbine Development Facing the Challenge of Future Energy
StructureTopics of Technical session• Aerodynamics•

Combustion• Transfer and Thermodynamics• Control, Diagnostics and Instrumentation Heat
• Innovative Clean/Renewable Energy Technology• Manufacturing Materials & Metallurgy• Structure and Dynamics•• Maintenance and User Experience

Applications

4

Location of Congress and Banquet Venue

Map to Shanghai Jiao Tong University, Minhang Branch Campus

 Direction Map from Pudong Airport / Hongqiao Airport to Shanghai Jiao Tong
University, Minhang Branch Campus

5

Map of Shanghai Jiao Tong University, Minhang Branch Campus

6 Congress Room in Chen Ruiqiu building
Main Congress Room is on the first floor.

Congress Rooms are on the second floor.

7 Banquet Venue
A cruise on the Huangpu River
Mingxin No.3 Cruise（in Chinese:名信号游船 3 号船）

Address:No.171, South Zhongshan Road, Shanghai( in Chinese:上海市中山南路 171 号）

8

Shuttle Bus Drive Route and Departure Time
Departure Time Drive Route
August 20,(Monday)

August 21,(Tuesday)August 22,(Wednesday)

06:40/07:00/07:20

Huating Hotel→ Graduate School of Shanghai Jiao Tong
University, Minhang Branch Campus (Hereinafter referred
to as “Congress Venue”)

12:15

Congress Venue→ Dazhiju Cafeteria

13:20

Dazhiju Cafeteria→ Congress Venue

17:45

Congress Venue→ Dazhiju Cafeteria

19:30

Dazhiju Cafeteria→ Huating Hotel/ Jianguo Hotel

07:40/08:00/08:20

Huating Hotel→ Congress Venue

12:15

Congress Venue→ Dazhiju Cafeteria

13:20

Dazhiju Cafeteria→ Congress Venue

17:20

Congress Venue→ Dada Wharf (Zhongshan South Road
171#, Near Fuxing East Road)

21:00

Dada Wharf→ Huating Hotel/ Jianguo Hotel

07:40/08:00/08:20

Huating Hotel→ Congress Venue

12:30

Congress Venue→ Dazhiju Cafeteria

13:30

Dazhiju Cafeteria→ Shanghai Turbine Plant (Minhang
District, Jiangshan Road 333#. Near Hongyuan Road)

16:30

1. Shanghai Turbine Plant→ Pudong Airport
2. Shanghai Turbine Plant→ Hongqiao Airport
3. Shanghai Turbine Plant→ Shanghai Branch of Chinese
Academy of Sciences

9Plant Tour

Introduction of Shanghai Turbine Plant

The Plant was Resources Commission General Machinery Co., Ltd. built on March 28,
1946. After foundation of the People’s Republic of China, it was named by the state Shanghai
Turbine Works, China’s first plant which designed and manufactured turbines. In 1955,
China’s first 6MW turbine was successfully manufactured by using Czechoslovak technology
and the plant was reputed as the “cradle of turbine in China”. In December 1995, Shanghai
Turbine Co., Ltd. was established with itself as the controlling shareholder as a Joint-Venturewith Westinghouse. In 1999 the equity of Westinghouse was transferred to Siemens and theplant became a global cooperative partner of Siemens. With an area of ca.1 km², the plant has
nearly 1200 sets of main equipment. Now affiliated to Shanghai Electric Power Generation
Equipment Co., Ltd., a Joint-Venture of Shanghai Electric and Siemens, the plant reached theannual production output of 36000MW in 2006, which ranked first in the world. Its domestic
market share approached nearly 40% and its products entered international markets. The plant
absorbed others’ advantages and innovated based on introduction of the world’s advanced
technology and management methods. 1000MW-class nuclear turbine and heavy duty gas
turbine were developed and manufactured. Introduced 300MW turbine reached the world’s
advanced level and was awarded the only gold quality prize of national high quality products
in China’s mechanical industry. 600MW-class turbine accomplished remarkableachievements. After operation of the first 1000MW-class ultra-supercritical turbine, whichreached world’s advanced level, it was awarded “the gold prize in China International
Industry Fair 2007” and “the special prize of China Mechanical Industry Science andTechnology 2009”.
STP is the first plant in China which has passed the qualification of ISO9001 Quality
Management System. Besides, it has passed the qualification of ISO14001 Environmental
Management System and OHSMS Occupational Health and Safety Management System. STP
has been honored with “National Model Enterprise in Establishing Harmonious Labor
Relationships”, “National Advanced Enterprise in Implementing Performance Excellence
Model”, “Home of National Model Staff”, “National Excellent Unit in Enterprise Culture
Construction”, “Top 500 Enterprises in China Mechanics”, “Leading Enterprise in China
Industry”, “National Advanced Unit in Enterprise Culture Construction in MechanicalIndustry”, “National Model Unit in Mechanical Industry” etc.
Shanghai Turbine Plant now takes the personal inspection of General-Secretary Hu
Jintao on July 28, 2004 as the motive force and is innovating and transforming to contributeto the development of power generation equipment manufacturing industry.

Workshop visit arrangement

1. Safety education
2. Gas Turbine Assembly Shop:
Visit Gas Turbine Assembly Shop on sightseeing platform, including component
assembly，rotor assembly and final assembly etc.



Brief Introduction of Gas Turbine Assembly Shop

The Gas Turbine Assembly Shop of STP was completed in September 29, 2010. The shop
is a manufacturing industrial base for heavy-duty gas turbine localization built by STP ,forspeeding up the “four changes”, enhancing the “five abilities”, building the “world-classfacility”, and invigoration of Shanghai Heavy equipment manufacturing industry.
Located along Huangpu River .It is a workshop of enclosed and temperature construction,with an area of 8733 square meters, 34 meters high, 46 meters wide, 168 meters long, an airtransport network with 9 cranes in three different layers, the maximum lifting capacity of thecranes is 350 tons. There are 8 "heavy" assembly platforms for gas turbine, steam turbine andnuclear steam turbine, and two vertical rotor stacking facilities, it can assembly the gas
turbine of E-class, F-class; HP-IP unit of combined-cycle steam turbine; High-pressure unit of10

1000MW nuclear steam turbine; HP-IP unit of 1000MW Ultra Super Critical steam turbine.
The Gas Turbine Assembly Shop has a world-class assembly capacity of power plant
equipment and will contribute the upgrading of Shanghai Electric Cooperation Group industry,
and the “re-starting” after changing the development mode.

11

Schedule at a GlanceAugust 20, 2012 （Monday）

08:00 - 18:00
09:15 - 09:30
09:30 - 10:20
10:20 - 10:35
10:35 - 12:15
12:15 - 13:30
13:40 - 15:15
15:15 - 15:30
15:30 - 17:35
18:00 - 19:30
Convention Hall
Convention Hall
5 rooms
Convention Hall
5 rooms

August 21, 2012 （Tuesday）

09:10 - 18:00
09:30 - 10:20
10:20 - 10:35
10:35 - 12:15
12:15 - 13:30
13:40 - 15:45
15:45 - 16:00
16:00 - 17:00
18:30 - 21:00
Registration
Opening Address
Keynote Speech 1
Coffee BreakTechnical Sessions
Lunch Break
Forum
Coffee BreakTechnical Sessions
Reception

Registration
Keynote Speech 2
Coffee BreakTechnical Sessions
Lunch BreakTechnical Sessions
Coffee BreakKeynote Lecture
BanquetConvention Hall
5 rooms
4 rooms
Convention Hall

August 22, 2012 （Wednesday）

09:10 - 12:00
09:30 - 10:20
10:20 - 10:35
10:35 - 12:15
12:15 - 12:30
12:30 - 13:45
13:45 - 16:30
18:00 - 20:30

Registration
Keynote Speech 3
Coffee BreakTechnical Sessions
Closing Address
Lunch BreakTechnical Tour
Committee Meeting

Convention Hall
4 rooms

SEC
CAS

12

Program Overview
Room A

Room B

Room CRoom D

Room E

Room F

202

203

204

205

206

CFD Analysis of
3D Flow (I)Advanced Gas
Turbine System(I)

Leakage Flow

Cooling andConjugate HT

Liquid and
Low-Btu fuels
Combustion (I)Unsteady Flowand Flow
Control (I)Innovative
Clean/Renewabl
e Energy
Technology

Centrifugal
Compressor

Rotor Dynamic
Analysis And
Lifetime
Prediction

Combustion
Numerical
Simulation

CFD Analysis of
3D Flow (II)Unsteady Flowand Flow
Control (II)Advanced Gas
Turbine System(II)

Film Cooling

Components
Aerodynamic
And Failure
Analysis (I)CFD Algorithm
and Modeling

Optimization
DesignAdvanced Gas
Turbine System(III)

Structure
Strength
Analysis And
Experimental
Investigation

Premixed
Combustion

Components
Aerodynamic
And Failure
Analysis (II)Cooling and HT
Enhancement

Liquid and
Low-Btu fuels
Combustion (II)Main Congress Room

100

9:15
9:30
9:30
10:20
Break

Aug.20(Mon)

Opening
Address
Keynote Speech
1

10:35
12:15
Lunch
13:40
15:15
Break

Forum

15:30
17:35
Closing
9:30
10:20
Break

Keynote Speech
2

10:35
12:15
Lunch
Aug.21
(Tue)

13:40
15:45
Break
16:00
17:00
Closing
18:30
21:00
9:30
10:20
Break

Aug.22(Wed)

Keynote Lecture
BanquetKeynote Speech
3

10:35
12:15
12:15
12:30
Lunch
13:45
16:30
18:00
20:30

Closing Address
Technical Tour (SEC)
Committee Meeting (CAS)13

Keynote and Forum Session
Keynote and Forum Session are held in Room A (Main Congress Room100)
 Keynote Lecture

August 21 (Tue) 16:00 - 17:00

Title: To be determined (he will summarize his 40 years effort to develop theadvanced gas turbine technology and new frames)
Prof. Sunao Aoki (Chief Research Fellow, Mitsubishi Research Institute, Inc., and Special adviser
to Mitsubishi Heavy Industries, Ltd.) Keynote Speeches
Keynote Speech 1

August 20 (Mon) 09:30 - 10:20

Title: To be determined
Speaker: Prof. Yasukata Tsutsui (the Ex-President of GTSJ)

Keynote Speech 2

August 21 (Tue)

09:30 - 10:20

Title: To be determined
Speaker: Prof. LI Ye (Director-General, Department of Energy Conservation and Scientific
Equipment, National Energy Administration)

Keynote Speech 3

August 22 (Wed) 09:30 - 10:20

Title: “Optimization of a Novel Film-Cooling Hole for Turbine Blade Cooling”
Speaker: Prof. Kwang-Yong Kim (Inha Fellow Professor, School of Mechanical Engineering,
Inha University)

 Forum Session

August 20 (Mon) 13:40 - 15:15“The Trends of Gas Turbine Development Facing the Challenge of Future Energy
Structure”

14Session ProgramAug.20 (Mon) am

Room A
Main Congress Room

100

9:15
9:30

Room B

Room CRoom D

Room E

Room F

202

203

204

205

206

CFD Analysis of 3D
Flow (I)

Advanced Gas
Turbine System (I)Leakage Flow

Cooling andConjugate HT

Liquid and Low-Btu
fuels Combustion (I)Chairperson:
From China

Chairperson:
Form Korea

Chairperson:
Form Japan

Chairperson:
From China

Chairperson:
From China

ACGT2012-1016
Numerical Study on the
Combination of
Simultaneous Adjustment
of Inlet Guide Vanes andDiffuser

ACGT2012-1003
Performance Prediction
for an Axial Compressorof an Industrial Gas
Turbine with Inlet Fogging

ACGT2012-1031
Numerical Investigation of
Unsteady Tip Clearance
Flow in a Low Speed
Axial Compressor

ACGT2012-4025
Aerodynamic
Performance of Purge
Flow Endwall Cooling inHigh Pressure Turbine
Cascade

ACGT2012-1102
Developing a model topredict droplet size andvelocity distribution of aliquid fuel swirl nozzle
spray

Tian Ye (Beijing Universityof Aeronautics andAstronautics, China), Hou
Anping, Shan Shujun, Ni
Qifeng

Chihiro Myoren (Hitachi
Research Laboratory,
Hitachi, Ltd. Japan),Tadaharu Kishibe, Takanori
Shibata and Yasuo
Takahashi

Baojie Liu, Bo Zhang,
Yangwei Liu (Beijing
University of Aeronautics
and Astronautics, China)

W Ghopa Wan Aizon(University of Iwate, Japan),Ken-ichiFunazaki,
TakemitsuMiura1

E. Movahednejad (MAPNA
Turbine Engineering &Manufacturing Co. (TUGA),
Iran,), A. Tabatabaei, A.R.
Ranjbaran

ACGT2012-1022
Numerical Simulation of
Four-Stage Gas Turbinewith Variable Gas
Properties

ACGT2012-1066
Power enhancement ofgas turbo-compressor ingas stations in hot and dry
climate with inlet air
cooling by use of cold
storage system

ACGT2012-1085
Passive Tip Clearance
Flow Control Using
Winglet for a Linear
Compressor Rotor
Cascade

ACGT2012-4026
Experimental andNumerical Investigations
on Aero-ThermalInteraction of Cooling Airs
Ejected from Multiple
Cooling Holes

ACGT2012-2065
Prediction of Sauter Mean
Diameter Based on
Energy Conservation Law

Qiang Xu (Shanghai ElectricPower Generation R & D
Center, China), Mei-bao
Zhang, Lian-hui Zhao, LeiHe

Ebrahim Khalili (National
Iranian Gas Company Shahrekord Gas Company,
Iran), Seyyed Mostafa
Hoseinalipour,EsmaeilHeybatian

Shaobing Han (Dalian
Maritime University, China),
Jingjun Zhong, Huawei Lu,
Xiaoxu Kan

Kamil Abdullah (Universiti
Tun Hussein Onn Malaysia,
Malaysia), Ken-Ichi
FunazakiChihiro Inoue (University ofTokyo, Japan), Toshinori
Watanabe, Takehiro
Himeno, Seiji Uzawa,
Mitsuo Koshi

ACGT2012-1029
Numerical Simulation of
the Effect of Inlet
Distortion to a Transonic
Axial-Flow Compressor
Rotor

ACGT2012-1072
Experimental
Investigation andAnalytical Study on the
Operation Performance ofa Small-sized Humid Air
Turbine Cycle

ACGT2012-1097
Investigation of Stability
Range Extension
Mechanism with Tip Air
Injection in a Low-Speed
Axial Compressor

ACGT2012-4033
Study on Conjugate Heat
Transfer and Stress of
Gas Turbine Blade

ACGT2012-2081
Effects of CO/H2 Molar
Ratio on Flame Structuresin Double-Swirled
Non-premixed Humid
Air/Syngas Burner

Fu Lei, Song Xizhen (Beijing
University of Aeronautics
and Astronautics, China), Li
QiushiChenyu Wei, Shusheng Zang
(Shanghai Jiao Tong
University, China)

Jichao Li (Institute ofEngineering Thermophysics,
Chinese Academy of
Sciences, China), Le Liu,
Zhiting Tong, Feng Lin,
Chaoqun Nie, Jingyi Chen

Yajun Song, Le Liu, Di
Zhang, Yonghui Xie (Xi’an
Jiaotong University, China)

Bing Ge (Shanghai Jiaotong
University, China), ShushengZang, Yinshen Tian

ACGT2012-1062
Numerical Analysis of theEffect of Dihedral on the
Performance of a Highly
Loaded TransonicCompressor Rotor

ACGT2012-1076
Performance Predictionand Simulation of Gas
turbine Inlet Air Coolingwith Inlet Fogging

ACGT2012-1060
Effects of the Axial Fins
Distance and Cavity
Depth on the Leakage
Flow Characteristics of
the Labyrinth Seal

ACGT2012-4109
Research on Conjugate
Heat Transfer of Turbine
Blade with Thermal
Barrier Coating

ACGT2012-2105
Numerical andExperimental
Investigation of a
Pressure-swirl Atomizer
SpraySong-lin Yu (Shanghai
Electric Power Generation
Group, China), Bin Wang,
Lian-hui Zhao, Lei He

J. Nagesh Kumar (National
Productivity Council, India),
T. Alwarsamy

Qing Gao, Yangzi Huang,
Jun Li (Xi’an Jiaotong
University, China), Zhenping
Feng, Lei He, Qiang Xu

Zhang Jingjing (Beijing
University of Aeronautics
and Astronautics,China),
Fang Xiangjun, Wang
Lianfu, Liu Siyong

Cunxi Liu (Institute ofEngineering Thermophysics,
Chinese Academy of Science,
China), Yanhui Mao,
Fuqiang Liu, Jinhu Yang,
Yong Mu, Gang Xu

Opening Address
Keynote Speech 1
Chairperson:
From China

9:30
10:20

10:35

11:00

11:25

11:50

12:15

Prof. Yasukata Tsutsui (theEx-President of GTSJ)

15

Aug.20 (Mon) pm

Room A
Main Congress Room

100

Room B

Room CRoom D

Room E

Room F

202

203

204

205

206

Unsteady Flow andFlow Control (I)Innovative
Clean/Renewable
Energy Technology

Centrifugal
Compressor

Rotor Dynamic
Analysis And
Lifetime Prediction

Combustion
Numerical
Simulation

Chairperson:
From China

Chairperson:
From China

Chairperson:
Form Japan

Chairperson:
From China

Chairperson:
From China

ACGT2012-1015
Effect of Circumferential
Single Grooved Casing
Treatment On Flow Fieldof Transonic Compressor

ACGT2012-5068
The Impact of the Wall
Thickness on the Outer
Wall Temperature in a
Tubular Solar Air
ReceiverACGT2012-1045
Behavior of Pressure
Fluctuation Rotatingaround Impeller Peripheryin A Centrifugal
Compressor Equippedwith Vaned Diffuser

ACGT2012-8001

ACGT2012-2021
Parametric CFD
Simulation of a Gas
Turbine Combustor

Yasunori Sakuma (Universityof Tokyo, Japan), Toshinori
Watanabe, Takehiro
Himeno, Dai Kato, Motohiro
ImaedaDunjin Wang (IET/CAS,
China), Feng Lin

Takashi Goto (Waseda
University, Japan), Atsuhito
Mizuno, Kazuyoshi
Miyagawa, Yutaka Ohta,
Eisuke Outa

M. S. Shahriary(Mavadkaran Eng. Co.,
Mapna Group, Iran), M.
Shahmiri, M. Cheraghzadeh

Duan Dong-Xia (Institute ofEngineering Thermophysics,
Chinese Academy of Science,
China), Cui Yu-Feng

ACGT2012-1082

ACGT2012-5134
Economic Assessment ofa Gas Turbine Combined
Heat and Power System
Using Biogas as Fuel

ACGT2012-1110
Numerical investigationon the mechanism of stallmargin improvement ofa centrifugal compressor

ACGT2012-8120
Three dimensional
numerical simulations for
estimation of burst speedof gas turbine disk

ACGT2012-2046
Optimization of the Fuel
Distribution in a DLN
Combustor by Simulation

Le Liu (IET/CAS, China),
Hongwei Zhang, Jichao Li,
Feng Lin, Chaoqun Nie

Jun Young Kang, Do Won
Kang, Tong Seop Kim (Inha
University, Korea), Kwang
Beom Hur, Jung Keuk Park

Liu Haiqing(IET/CAS,
China), Gao Chuang , Geng
Shaojuan, Zhang Hongwu

Tirumala Rao Koka
(Honeywell Technology
Solutions Lab Pvt. Ltd., India),
Ramachandra Krishnaswamy

Kun Wang (IET/CAS,
China), Yufeng Cui, Aibing
Fang, Chaoqun Nie

ACGT2012-1090
Peak Efficiency
improvement of aTransonic Fan Rotor by
Shaping Circumferential
Casing Grooves

ACGT2012-9127
Investigation of gas
turbines for concentrating
solar power applications

ACGT2012-1117
An investigation on the
Flow-induced Noise
Characteristics ofCentrifugal compressor

ACGT2012-8129
Rotor dynamic analysis ofa large turbo generator
applying finite element
methodACGT2012-2077
Large Eddy Simulation of
an Industry Gas-Turbine
Model Combustor Using
REDIM Technique

Xi Nan (IET/CAS, China),
Juan Du, Feng Lin, Jingyi
Chen

Mojtaba Bozorgmehr(Tarbiat Modares
University, Iran)

Taebin Jeong (Seoul
National University, Korea),
Chanyoung Lee, Kyoung-ku
Ha, Shin-hyoung Kang

Hossein Badr Rezaei(Mapna Turbine Engineering& Manufacturing Co. Iran),Aboozar Shaebani

P. Wang (Jiangsu
University, China)

ACGT2012-1083
Low Speed Axial
Compressor Stall Margin
Improvement by Unsteady
Plasma Actuation

ACGT2012-2103
Influence of different
carbon capture
technologies on theperformance of the
combined cycle power
plant

ACGT2012-1093
Aerodesign and Flow
Field Analysis of a High
Transonic
Impeller with Total
Pressure Ratio 12.0

ACGT2012-6091
Development of Rough
MCrAlY Bond Coat in
Thermal Barrier Coatings
System

ACGT2012-2079
Numerical Analysis of Exit
Temperature Profile of a
Gas Turbine Combustor

Li Gang (IET/CAS, China),
Yang Lingyuan, Nie
Chaoqun, Zhu Junqiang, Xu
Yanji, Sergey Leonov

Ji-Ho Ahn, Tong Seop Kim(Inha University, Korea)

Chuang Gao (Shanghai
Advanced Research Institute,
Chinese Academy of
Sciences,China), Weiguang
Huang, Hongwu Zhang

Yongqing Wang
(Chromalloy, USA), Matthew
Wilson, Gerard W
Milidantri, Mahinda
Wanigasinghe

Fan Fan (Tsinghua
University, China), Haiying
Qi, Chong Feng, Junzong
Zhu

ACGT2012-1088
Investigation of boundary
layer development in Low
Pressure Turbine Cascadeswith unsteady incoming
wakes – Effect of Reynolds
Number

ACGT2012-8098
Application of
Diffusion-Brazing Repair
Technology for Land-base
Gas turbine Nozzles

ACGT2012-2135
Time-dependent motion in
one turbulent swirling
non-premixed flame

Ayumi Mamada (IHI
Corporation, Japan),
Hidekazu Kodama, Kazuki
Okamura, Ken-ichi Funazaki

Daizo Saito (Toshiba
Corporation, Japan), Yomei
Yoshioka, Kazuhiro
Kitayama, Yoshiaki Sakai

Yang Yang, Xiaodi Tang
(IET/CAS, China)

Forum

13:40
15:15

15:30

15:55

16:20

16:45

17:10

17:35

The Trends of Gas
Turbine Development
Facing the Challenge of
Future Energy Structure

Effects of Single
Circumferential Groove at
Different Axial Locations on a
Low-Speed Axial
Compressor’s Tip Region
Flow

16

Assessment ofservice-induced
microstructural andmechanical properties ofNimonic 80A turbine blade
and its lifetime prediction

Aug.21 (Tue) am

Room A
Main Congress Room

100

Room B

Room CRoom D

Room E

Room F

202

203

204

205

206

CFD Analysis of 3D
Flow (II)Unsteady Flow andFlow Control (II)Advanced Gas
Turbine System (II)Film Cooling

Components
Aerodynamic And
Failure Analysis (I)Chairperson:
From China

Chairperson:
From China

Chairperson:
Form Japan

Chairperson:
From China

Chairperson:
From China

ACGT2012-1080
Computation ofParticulate Erosion in a
Jet Engine Fan

ACGT2012-1058
Experimental Study on
Plasma Aerodynamic
Control for Improving
Wind Turbine
Performance

ACGT2012-2119
The Improved Air Cooled
Combustor for Mitsubishi
G Class Gas Turbine

ACGT2012-4004
Effects of CO2 Coolant
Mass Fraction on the Film
Cooling Performance ofGas Turbine Blade

ACGT2012-8010
Aerodynamic Numerical
Simulation of a Failure
Three-Stage Centrifugal
Compressor

Masaya Suzuki (Japan
Aerospace Exploration
Agency, Japan), Makoto
Yamamoto

Hisashi Matsuda (TOSHIBA
Corporation, Japan),
Motofumi Tanaka, Shohei
Goshima, Kiyoyuki
Amemori, Masahiro
Nomura, Toshiki Osako

Keizo Tukagoshi, Satoshi
Tanimura, Koichi Nishida,
Keijiro Saitoh, Hiroaki
Kishida, Kentaro Tokuyama(Mitsubishi Heavy
Industries, ltd, Japan)

Sang-Gwon Kim,
Sung-Ryong Lee, Youn-Jea
Kim (Sungkyunkwan
University, Korea)

GUI Xing-min (Beihang
University, China), Meng
Xiang-wei, Wei Bao-feng,
JIN Dong-hai

ACGT2012-1084
Simulation of a Gas
Turbine Cascade within
the Full Test Cell
Environment

ACGT2012-1061
Study on Vortical
Structure of Separation
Flow Control Using
Synthetic Jets on a
High-lift Low-pressure
Turbine Blade

ACGT2012-7138
Verification Test Of Newly
Developed High Efficient
30mw Class Gas Turbine
The Kawasaki L30a

ACGT2012-4075
Film Cooling Prediction on
a Turbine Vane using
Algebraic Anisotropic
Eddy Viscosity Method

ACGT2012-8017
Multimode Flutter
Analysis based on
Time-Domain Fluid-Solid
Interaction Simulation and
System Identification

R O Evans, Q Zhang, W
Chen, W N Dawes(Cambridge University
Engineering Department,
UK), C F Favaretto

Ye Dongting (Shanghai
Turbine Works, China), He
Haiyu, Xie Yonghui, Shen
Guoping, Lu Wei

Ryozo Tanaka (Kawasaki
Heavy Industries, LTD.,
Japan), Koji Take, Masanori
Ryu, Akinori Matsuoka,
Atsushi Okuto

Li Xueying (Tsinghua
University, China), Ren Jing,
Jiang Hongde

Atsushi Tateishi (Universityof Tokyo, Japan),Toshinori Watanabe,
Takehiro Himeno

ACGT2012-1094
Mechanism Research of
End-Wall Flow Responseto the Inlet Total Pressure
Distortion in a SupersonicCompressor

ACGT2012-1099
Reduction of Supersonic
Jet Noise With Impinging
Microjet

ACGT2012-9108
Development of 1.7MW
Class High Efficiency Gas
Tur bine M1A-17

ACGT2012-4086
Numerical Investigation ofFilm Cooling Using a
Chemical Heat Sink

ACGT2012-8020
Failure Analysis forCompressor S1 Vane of
PG9351FA Gas Turbine

Sun Peng (Dalian Maritime
University, China), Gao
Haiyang, Du Kun, Zhong
Jingjun

Ryuichi Okada (University ofTokyo, Japan), Toshinori
Watanabe, Seiji Uzawa,
Takehiro Himeno, Tsutomu
Oishi

Yasufumi Hosokawa(Kawasaki Heavy Industries,
LTD., Japan), Takahiro
Nakasuji, Yoshihiro
Yamasaki, Makoto Gouda

Keyong Cheng (Institute ofEngineering Thermophysics,
Chinese Academy of
Sciences, China), Shiqiang
Liang, Xiulan Huai, Wei
Chen, Yongxian Guo

Junfeng Xiao (Xi’an Thermal
Power Research InstituteCo., Ltd., China), Song Gao,
Xiaobing Yu, Yonghai
Zhang, Weiwei Gu

ACGT2012-1118
Effects of Surface
Roughness and Adverse
Pressure Gradient on
Turbulent Boundary Layer
Characteristics

ACGT2012-1126
Reynolds Number Effects
on Flow Separation
Control of Low-Pressure
Turbine Using Plasma
Actuators

ACGT2012-9115
Development and Test
Results of a New 1600
degreeC Turbine Inlet
Temperature J Series
Gas Turbine

ACGT2012-4123
Effect of Wall Curvature
on Film Cooling Flows
Along a 1st Stationary
Vane

Ju Hyun Shin, Semin Jang,
Seung Jin Song (Seoul
National University, Korea)

Takayuki Matsunuma(National Institute ofAdvanced Industrial Scienceand Techonology, Japan),
Takehiko Segawa

Yuji Komagome (Mitsubishi
Heavy Industries, LTD,
Japan), Satoshi Hada,
Masanori Yuri, Junichiro
MasadaHideyuki Sakamoto,Kenichiro Takaishi (Osaka
University, Japan), Yutaka
Oda, Tetsuji Nagao

Keynote Speech 2
Chairperson:
Form Korea

9:30

10:20

10:35

11:00

11:25

11:50

12:15

Prof. LI Ye(Director-General,
Department of Energy
Conservation and Scientific
Equipment, National Energy
Administration)

17

Aug.21 (Tue) pm

Room A
Main Congress Room

100

Room B

Room CRoom D

Room E

202

203

204

205

CFD Algorithm andModeling

Optimization Design

Advanced Gas Turbine
System (III)Structure Strength
Analysis And
Experimental
Investigation

Chairperson:
Form Korea

Chairperson:
From China

Chairperson:
From China

Chairperson:
Form Japan

ACGT2012-1028
Studies on Unsteady
Characteristics of Corner
Separation in a Compressor
Cascade based on Hybrid
LES/RANS Methods

ACGT2012-1011
Optimization of Endwall
Contouring in Axial
Compressor Transition Duct

ACGT2012-4002
Thermodynamic
Investigation of Typical
25MW Simple Cycle Gas
Turbine and EffectivenessEvaluation of Intercooler,
Reheat and Regenerator

ACGT2012-8053
Conjugate Heat Transfer andStress Analysis of Vanes in a
Gas Turbine

Zhong-Nan Wang (Tsinghua
University, China), Xin Yuan

Zhao Wei-Guang (Beihang
University, China), Jin
Dong-Hai, Gui Xing-Min

Shahrokh Sorkhkhah (MAPNA
Turbine Engineering &Manufacturing Company, Iran),
M.R.shahrifabadi

Heeyoon Chung, Jun Su Park,
Hokyu Moon, Sanghoon Lee,
Hyung Hee Cho (Yonsei
University, Korea)

ACGT2012-1056
Implementation andValidation of the
Spalart-Allmaras Turbulence
Model in TransonicCompressor FlowsACGT2012-1014
Aerodynamic Optimization
Design of TurbomachineryCascade Based on Discrete
Adjoint Method

ACGT2012-4024
Dynamic Simulation
Saturated Steam toSuperheated steam Processin Superheater on PT. BOC(British Oxygenate
Company) Gresik Power

ACGT2012-8107
Coupling Method between
Conjugate Heat Transfer
Simulation and Thermal
Stress Analysis

Yangwei Liu (Beijing Universityof Aeronautics and Astronautics,
China), Baojie Liu, Lipeng Lu

Chaolei Zhang (Xi’an Jiaotong
University, China), Juan Lu,
Zhenping Feng

Dewi Anggraeni (PUSTEKBANG,
LAPAN, Indonesia), DR. Totok
Suhartanto

Takashi Yamane (Japan
Aerospace Exploration Agency,
Japan)

ACGT2012-1064

ACGT2012-1047
A Numerical Investigation on
Parameterized Sweep
Design Impacting on the
Aerodynamic Performance ofTransonic Fans

ACGT2012-5040
Introduction to GT and GT
Auxiliary Equipments in
Some IGCC Power Plant

ACGT2012-8131
Fir-Tree Tenon/Mortise
Structure Design Under RealAero-Engine Turbine
Environment Based On UG
and ANSYS

Jian Fang (Beihang University,
China), Zhaorui Li, Lipeng Lu

Ren Peng (Beijing University of
Aeronautic and Astronautic,
China), Yuan Wei

Zhang Qiu-Chi (Shanghai
Electric Power Generation
Equipment Co., Ltd., China),
Zhang Dong-Fang

Yang XiaoJie (IET/CAS, China),
Du Qiang, Zhu JunQiang

ACGT2012-1114
Investigation Of Large Eddy
Simulations For Internal Flow
Using New
Flux-Reconstruction High
Order Method

ACGT2012-1063
An Aerodynamic
Optimization System For
Axial-Flow Turbines

ACGT2012-5051
Performance Analysis of a
400MW SOFC/IGCC
Combined System

ACGT2012-8136
An Experimental
Investigation of the Last
Stage Vibration Stress of an
Actual Size Steam Turbine in
Various Low Load Conditions

Yi Lu (Tsinghua University,
China), Kai Liu, Xin Yuan ,W.N.Dawes

Xiao-Dong Zhang (IET/CAS,
China), Jian-Jun Liu, Yun-Tao
Zeng

Ma Zheshu (Jiangsu Universityof Science and Technology,
China), Xu Chen

Naoki Shibukawa (Toshiba
Corporation, Japan), Yoshifumi
Iwasaki, Mitsunori Watanabe

15:20

ACGT2012-1101
Numerical Study on a
Boundary Source Method forSimulating the Effect of
Shroud Cavity Flow in an
Axial Turbine

ACGT2012-1067
Highly Loaded Aerodynamic
Design of the Helium
Compressor

ACGT2012-1070
Numerical Study on a Kiel
Probe Used in Rotor Wake ofa High Speed Axial
Compressor

ACGT2012-3140
Error Analysis andCompensation of a
Four-Coordinate Measuring
System for Turbine Blades

15:45

Mao Ning, Zhang Dongyang(IET/ CAS, China)

Tingfeng Ke (Shanghai
Advanced Research Institute,CAS, China), Jingxuan Zhang

Sichen Wang (IET/CAS, China),
Scott C. Morris, Kai Wang,
Feng Lin

Jianlu Wang (Dongfang Steam
Turbine Co., Ltd., China), Lei
Chen, Xueyun Liu, Huajie Liu,
Bing Li

13:40

14:05

14:30

Direct Numerical Simulation of
Shock/Turbulence Interaction
by Using Low-Dissipative
Monotonicity-Preserving
Scheme

14:55

Keynote Lecture
Chairperson:
From China

16:00
17:00

Prof. Sunao Aoki (Chief
Research Fellow, Mitsubishi
Research Institute, Inc., andSpecial adviser to Mitsubishi
Heavy Industries, Ltd.)18

Aug.22 (Wed) am

Room A
Main Congress Room

100

Room B

Room CRoom D

Room E

202

203

204

205

Premixed Combustion

Components
Aerodynamic And
Failure Analysis (II)Cooling and HT
Enhancement

Liquid and Low-Btu
fuels Combustion (II)

Chairperson:
From China

Chairperson:
Form Korea

Chairperson:
From China

Chairperson:
Form Japan

Keynote Speech 3

9:30

10:20

10:35

11:00

11:25

11:50

12:15

Chairperson:
Form Japan
Optimization of a Novel
Film-Cooling Hole for
Turbine Blade CoolingProf. Kwang-Yong Kim ( Inha
University, Korea)

ACGT2012-2009
Experimental Study on Flow
Losses of Cavity-Base Strut
Flame Stabilizer

ACGT2012-8049
Characteristics of Gas
Journal Bearings in Micro
Gas Turbine Considering
Rarefaction Effect

ACGT2012-4122
Heat Transfer Enhancementof Impinging Jet Cooling by
Circle-Rib

ACGT2012-2019
Non-equilibrium Plasma
Assisted Combustion of
Low-BTU Fuels in a Gas

Liu Denghuan (Beihang
University, China), Jin Jie

Haijun Zhang (Jiaxing
University, China), Qin Yang

Yuichi Ichikawa (Osaka
University, Japan), Kenichiro
Takeishi, Yutaka Oda, Kiyoshi
SugetaHongbin Hu (IET/CAS, China),
Gang Li

ACGT2012-2012
Experimental investigation of
dynamic and emission
characteristics of a dry low
NOX gas turbine combustor

ACGT2012-4054
The Sensitive Parameter
Study of Axial Flow
Compressor Fouling

ACGT2012-4078
Rib Induced Heat Transfer
Development inside a Gas
Turbine Internal Cooling
Channel

ACGT2012-2044
Development of Leading
Technology for a Low-BTU
Gas-firing Gas-turbine
Combined-cycle Plant at a
Steelworks

Xing Shuang-xi (IET/CAS,
China), Fang Ai-bing, Song
Quan-bin, Cui Yu-feng, Nie
Chao-qun

Yang Hua-dong (North China
Electric Power University,
China), Xu Hong

Kan Rui (Tsinghua University,
China), Yang Li, Ren Jing, Jiang
HongdeToyoaki Komori, Koichiro
Yanou, Takashi Kishine,
Nobuyuki Yamagami, Yutaka
Shimamura (Mitsubishi Heavy
Industries, Ltd., Japan)

ACGT2012-2042
Combustion Instability
Analysis based on a
Low-order Ther-moacoustic
Model for Premixed Swirling
Flame

ACGT2012-4142
Three-dimensional numericalsimulation of non-uniform
growth of the thermallygrown oxide in thermal
barrier coating systems

ACGT2012-4095
Pressure loss and Heat
Transfer in channels with pin
fin-dimple combined arraysfor gas turbine coolingapplication

ACGT2012-2121
Application of Bio-Fuel in aSingle-Sector Combustor fora Small Experimental
Aero-Engine

Yang Fujiang (BeiHang
University, China), Guo Zhihui

Yan Wang (Dongfang TurbineCo., Ltd , China), Luochuan Su,
Weixu Zhang, Tiejun Wang

Yu Rao (Shanghai Jiaotong
University, China), Xiang
Zhang, Chaoyi Wan

Keiichi Okai (Japan Aerospace
Exploration Agency, Japan),Hitoshi Fujiwara, Motoyuki
Hongoh, Kazuo Shimodaira

ACGT2012-2074
Performance Test of a DLN
Combustor on Emission andTemperature Traverse
Quality

ACGT2012-4052
Heat transfer characteristics
of impingement/effusion
cooling on a concave duct

ACGT2012-1143
CFD Study on Double Radial
Swirlers in Combustor

Junzong Zhu, Haiying Qi(Tsinghua University, China),
Chong Feng

Eui Yeop Jung, Chan Ung Park
Dong Hyun Lee, Kyung Min
Kim, Hyung Hee Cho (Yonsei
University, Korea)

Song Ai (Dong Fang TurbineCo., LTD., China), Yong Yang,
Gang Xie, Jian Tao

19

General Information


Language

The official language of ACGT2012 is English.

Registration and Information Desk

Aug. 20 (Mon)Aug. 21 (Tue)Aug. 22 (Wed)

08:00 - 18:00
09:10 - 18:00
09:10 - 12:00
at 2nd floor in “Chen Ruiqiu Building”

For Speakers in Technical Sessions

1. Author biography form
Presenting authors, who haven’t submitted the biography form to chairperson, should fill out theform and hand it over to chairperson before their sessions start.

2. Arrival at the session room
All speakers should arrive at their session rooms well before their sessions start. Authors who will
use the beam projector can upload the presentation files to the PC equipped in the room. Authors canuse their own PC on their own responsibility. All the time required for the computer setting forpresentation will be included in their presentation time.

3. Presentation time
25 minutes, including 5 minutes for discussion, are allotted to each presentation.

For Chairperson in Technical Sessions

Session chairpersons should arrive at the session room well before the session begins. Check if allpresenting authors come and their biography forms have been submitted. Please keep the allocatedpresentation time and allow sufficient time for discussion.

Registration

The registration fee is USD250 (USD100 for students). The registration fee includes access to all
sessions, final program with paper abstracts, USB proceedings, daily working lunches, banquet, coffee
breaks, shuttle bus between xujiahui district and congress venue.

Proceedings
A USB flash disk including all the full papers of ACGT2012 will be distributed to all registrants.



Wireless Network

Mobile devices such as notebook computer, mobile phone and Ipad etc. are able to connect towireless networks in conference room, teaching building and laboratory building on campus.
The name of wireless network is: “SJTU”.
There are two login ID:
1. ID：ACGT20121
PASS：3320prkr
2. ID：ACGT20122



PASS：3743ohct

Lunch

Restaurant is located next to the Academic Activities Center. Walk needs about 15 minutes, there
are shuttle bus to and from restaurant and congress venue.

20