2018.3.15.Mingxiao Hall

Open Ceremony

L-1 Plenary Lecture

L-2 Plenary Lecture

8:30-9:00

9:00-9:40

9:40-10:20

Break10:20-10:50

C-1 Propulsion & Power componentsSession A-1 Computational Methods B-1 Fundamentals D-1 Propulsion & Power systems

10:50-11:10

11:10-11:30

11:30-11:50

11:50-12:10

AJCPP2018-011Validation of impedance eduction method for acoustic liner panel in grazing flow

Takuya Harada (The University of Tokyo)

Propulsion system of Chinese new generation launch vehicleRuixiang Fan（China Academy of Launch Vehicle Technology）

Opportunities and Challenges in Commercial Aero Engine DevelopmentJinzhang Feng (AECC Commercial Aircraft Engine Co., LTD)

AJCPP2018-013Dynamic Simulation of Hypersonic Pre-cooled Turbojet Engine

Kazuki Kaneoya (Waseda University)

AJCPP2018-001Study for Performance Improvement of Ejector with Mixer Lobes in Annular Duct Subsonic Flow

Kenji Kobayashi (Sojo University)

AJCPP2018-005AIRCRAFT IN A SUSTAINABLE SOCIETY

Masako Shishido(Iwate University)

AJCPP2018-019Comparison of the Linear and Non-linear Unsteady Aerodynamic Forces on the Vibrating Blade Row

Christopher Naval (Kyushu University)

AJCPP2018-029Effects of composition on laminar burning velocity of propane/air/dilution gas mixtures under combustion engine conditions

Masamichi Matsuura (Osaka Prefecture University)

AJCPP2018-003Numerical Study of Inlet Performance with Airframe/Propulsion Interference for High Mach Integrated Control Experiment “HIMICO"

Hidekazu Yoshida (Waseda University)

AJCPP2018-006Optimization Design of the Capacitance Void Fraction Sensor adopting Multi Asymmetric Electrodes for Two Phase flow

Yo Nakajima(Waseda University)

AJCPP2018-020Simple Non-Reflecting Mixing-Plane Method for Multi-Stage Turbomachinery CFD with Improved Conservation

Naoki Tani (IHI)

AJCPP2018-040Combustion Characteristics of the Methane-Oxygen Diffusion Flame According to the Injector-type Variation

Joon Yeol Hong (Pukyong National Universi-ty)

AJCPP2018-004Numerical Estimation for Surface Erosion of Solar Arrays on a Geostationary Satellite by Hall Thruster Plume Spacecraft Interactions

Takanobu Muranaka (Chukyo University)

AAJCPP2018-008The Study on Performance Improvement of a Tip-Driven Electromagnetic Fan for Aircraft Propulsion using a Lab-Scale Model

Shoichi Abe (Nihon University)

AJCPP2018-021Numerical Investigation of Novel Tesla Turbine Concept Combined with a Cascade

Shogo Nishimura (The University of Tokyo)

AJCPP2018-049The characteristics of weak shock waves propagating through a convergent channel

Guang Zhang (Andong National University)

AJCPP2018-031Modal Analysis of Combustion Oscillation Based on High-speed Measurements of CH* chemiluminescence for a Liquid Rocket Engine Model Combustor with a Pintle Injector

Kyo Sugihara (The University of Tokyo)

AJCPP2018-017Proposals for small Propulsion & Power systems using tetra-ol GAP

Ayana Banno (Chiba Institute of Technology)

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Mingxiao Hall QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

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GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

13:30-13:50

13:50-14:10

Lunch Time12:10-13:30

AJCPP2018-025Sound Absorption Characteristic of Stainless Steel Foam with Porosity Variation

Jannati A. Tuasikal (The University of Tokyo)

AJCPP2018-054Drag Reduction of Hypersonic Blunt Body by Reacting/Non-reacting Gas Injection

Yong-Chan Kim(Inha University)

AJCPP2018-033Effect of Inlet Distortion on Aerodynamic Characteristics of Axial Fan

Ryuichi Okamoto(The University of Tokyo)

AJCPP2018-022Conceptual Study on PEFC-LiB Hybrid Propulsion System

Takayuki Kojima(JAXA)

AJCPP2018-027Numerical Analysis of the Effect of Cathode Configuration on Hydrogen MPD Thruster Performance

Shitan Tauchi(The Graduate University for Advanced Studies)

AJCPP2018-056Analysis of Injection Conditions of Counter-flow Jets for Drag Reduction of a High Speed Vehicle

Jaecheong Lee(Chungnam National Universi-ty)

AJCPP2018-037System Parameter Influences on Explosive Detonation in Microscale Exploding Foil Initiator

Kyoungjin Kim(Kumoh National Institute of Technology)

AJCPP2018-023Development of Electrothermal Pulsed Plasma Thruster Systems for Powered Flight onboard the Osaka Institute of Technology 2nd PROITERES Nano-Satellite

Ryota Fujita(Osaka Institute of Technology)

14:10-14:30

14:30-14:50

AJCPP2018-028Numerical Flow Simulation of Multiple Resonators under 2D Grazing Flow

Tsubasa Iwafune(Kanazawa Institute of Technology)

AJCPP2018-057Dependency of Supersonic Combustion Regimes on Fuel Temperature

Jeong-Yeol CHOI(Pusan National University)

AJCPP2018-038Ultrasonic Atomization Effect on Partial-ly-premixed Combustion of Kerosene-Air Mixture Sprayed through a Slit-jet Nozzle

Min Cheol Kim(Pukyong National Universi-ty)

AJCPP2018-024Development of the Osaka Institute of Technology 2nd PROITERES Nano-Satellite with High-Power Electrothermal Pulsed Plasma Thrusters for Powered Flight

Ryota Fujita(Osaka Institute of Technology)

14:50-15:10

AJCPP2018-032Large Eddy Simulation of turbulent combus-tion in Precooled Turbojet Model Afterburner using Eddy Dissipation Concept

Hiromu Ishikawa(The University of Tokyo)

AJCPP2018-068Effect of Particle Damping for Solid Rocket Motors Considering Tri-modal Particle Size Distribution

Donghee Lee(Korea Aerospace University)

AJCPP2018-046Study on Performance Analysis of Solid Rocket Motors using Multi-Dimensional Modules

Seok-Hwan Oh(Inha University)

AJCPP2018-058Preliminary Performance Estimation of 50 W-class RF Ion Engine

Pham Tran Dang Quang(University of Ulsan)

15:10-15:30

AJCPP2018-035LES investigation of supersonic mixing layer using different type of gas

Tatsuya Kishi(Okayama University)

AJCPP2018-070Viscosity and Viscoelastic properties of Mono-propellant Gel with Nano/Micro Sized SiO2 Gellant

Jinwu Jang(Korea Aerospace University)

AJCPP2018-047Flame Characteristics of Gaseous Fuel / LOx Combustor at Supercritical Pressure

Tae Seon Park(Kyungpook National University)

AJCPP2018-016Engine-Cycle Analysis on Boundary Layer Ingesting Engine Reflecting Experimental Data with Distortion Plate

Yoshihiro MITANI(Waseda University)

AJCPP2018-030Swirling Combustion Flow Field Evaluation of Tangential-Axial Injection Hybrid Rocket by Large Eddy Simulation

Tomoki Matsuno(The University of Tokyo)

AJCPP2018-063Prediction of Pseudo Shock Waves in a Constant Area Duct

Vignesh Ram Petha Sethuraman(Andong National University)

AJCPP2018-039Performance Characteristics of the Bipropel-lant Methane Thruster Using Swirl-coaxial Injector

Seong Hun Bae(Pukyong National Universi-ty)

AJCPP2018-034Key Technologies for Microwave Rocket

Kuniyoshi Tabata(The University of Tokyo)

C-2 Propulsion & Power componentsSession A-2 Computational Methods B-2 Fundamentals D-2 Propulsion & Power systems

Break15:30-15:50

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GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

15:50-16:10

16:10-16:30

AJCPP2018-078Turbulence Model Selection and Parameter Optimization for Micro-scale Compressor Performance Simulation

Zhiping LI(Beihang University)

AJCPP2018-073Development of Hypersonic Ludwieg Tube of Konkuk University(KULT)

Sungmo Yang(Konkuk University)

AJCPP2018-048Flow Separation Characteristics of An Asymmetric Nozzle

Kang-min Lee(Korea Aerospace University)

AJCPP2018-081Analysis of Thermal Throat Characteristics of a Wide-Range RBCC Combustor at Ramjet ModeLUO Feiteng(Science and Technology on Scramjet Laboratory Beijing Power Machin-ery Research Institute)

AJCPP2018-083New realization of CFD turbulence simulation

Mikhail Ja. Ivanov(Central Institute of Aviation Motors)

AJCPP2018-084Stall Warning Approach with Complicated Inlet Flow

Ruize Xu(Beihang University)

AJCPP2018-053Swirl Injection and Combustion Instability in Hybrid Rocket

Jungeun Kim(Konkuk University)

AJCPP2018-098Effects of Flow Condition and Injector Geometry on Flame Structure from Bi-swirl Coaxial Injectors

Donghyun Hwang(Chungbuk National University)

16:30-16:50

16:50-17:10

AJCPP2018-085A Hybrid Method for Lean Blow-off Predictions of Swirling Stabilized Flames

Zhonghao Wang(Chinese Academy of Sciences)

AJCPP2018-104POD Analysis of Surface Wave Characteris-tics on Conical Liquid Film

Zhongtao Kang(CARDC)

AJCPP2018-059Study on Multiple Shock Waves in a Supersonic Nozzle

Jintu K. James(Andong National University)

AJCPP2018-103Design of a tri-ducts inward turning inlet for a wide-range operation with a single rotational flap

Chengxiang Zhu(Xiamen University)

17:10-17:30

AJCPP2018-089Large Eddy Simulation of Supersonic Turbulent Boundary Layer over a Shock-elim-inating Wavelike Wall

Xu Wang(National University of Defense Technology)

AJCPP2018-125Investigation on flow characteristic and parameters optimization of a new conception of hybrid TC nozzle

Fu Song(Northwestern Polytechnical University)

AJCPP2018-072Analysis of Turbulent Combustion Character-istic of Single Rocket Combustor with Shear-coaxial GH2/GO2 Injector

Seung-Min Jeong(Pusan National University)

AJCPP2018-165Air Turbo Ramjet Expander Performance AnalysisBased on Gases Dissociation Effect

Chen Huan(CAS)

17:30-17:50

AJCPP2018-091Large Eddy Simulation of the Flow Structures and Mixing Fields in a Rear-wall-expansion Cavity

Zun Cai (Science and Technology on Scramjet Laboratory)

AJCPP2018-128Numerical Simulations of Shock-Induced Combustion for Hypersonic Air-Breathing Propulsion

Sheng Zhang (Tsinghua University)

AJCPP2018-090Study on Boundary Layer Flow Regime of Diffusion Cascade

LM Gao (Northwestern Polytechnical University)

AJCPP2018-012Combustion Test of Hydrocarbon Fueled Ramjet Combustor

Hideyuki Taguchi (JAXA)

17:50-18:10

AJCPP2018-101Development of a 1D Method for Hall Thruster Performance Analysis

Mingyoung Cho (Korea Aerospace Universi-ty)

AJCPP2018-129Study about the Influence of Exit Shape on the REST Inlet during Cross Section Fusion Process

Shuai Zhou (Aero Engine Academy of China)

AJCPP2018-092Shape Control and Surface Hydrophilic Modification of Emitter Arrays for Ionic Liquid Ion Source Electrospray Micro Thruster

YU M. Xing (Beihang University)

AJCPP2018-014Experimental and Analytical Study on Suppression of Blade Vibration using Tip-Located Electromagnetic Device

Keiichi OKAI (JAXA)

AJCPP2018-088Investigation on The Vibration Energy Transmission Mechanism of Casing with Different Load and Boundary Conditions Based on Structural Intensity Method

Yingqun Ma(Chinese Academy of Sciences)

AJCPP2018-116Study on the influence of the fluid-ther-mal-structural coupling on the inlet parame-ters of the hypersonic intake

Guangyue Dai(China Aerodynamics Research and Development Center)

AJCPP2018-061Analysis of Single Radial Swirler Combustor by Using DMD(Dynamic Mode Decomposi-tion)

Kyobin Lee(Korea Aerospace University)

AJCPP2018-149Technique of Investigation of Thermal Conductivity of Materials In a Field of Centrifugal Accelerations

Alexander Lepeshkin(Central Institute of Aviation Motors)

C-3 Propulsion & Power componentsSession A-3 Computational Methods B-3 Fundamentals D-3 Propulsion & Power systems

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GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

2018.3.16.Mingxiao Hall

L-3 Plenary Lecture

L-4 Plenary Lecture

8:30-9:10

9:10-9:50

Break9:50-10:20

C-4 Propulsion & Power componentsSession A-4 Computational Methods B-4 Fundamentals D-4 Test and Evalution

13:30-13:50

13:50-14:10

14:10-14:30

AJCPP2018-105Numerical Investigation of Diffuser Rotating Stall in a Centrifugal Compressor with Vaned Diffuser

Yang Zhao (Xi’an Jiaotong University)

R&D Activities on Aero-propulsion and Power in JapanToshinori WATANABE（The University of Tokyo）

Overview of a Pintle Injector for Liquid Rocket EnginesJaye Koo （Korea Aerospace University）

L-5 Plenary Lecture

L-6 Plenary Lecture

10:20-11:00

11:00-11:40

Lunch11:40-13:30

Progress in Hypersonic Airbrething PropulsionRiheng Zheng(Science and Technology Laboratory on Scramjet)

Volcanic Ash: a fundamental propulsion hazard?Donald Dingwell(Ludwig-Maximilians-University Munich)

AJCPP2018-133Research on impact force measurement based on stress wave

Zongjin Ren (Dalian University of Technolo-gy)

AJCPP2018-093Numerical Investigation on Rotating Instability in a Transonic Fan Rotor

Ming Zhang (Beihang University)

AJCPP2018-036A ground combustion test facility for high altitude simulation

Isang Yu (Chungnam National University)

AJCPP2018-110Numerical Simulations Aided Diagnostic of the Flow in JF-16 Expansion Tube

Kai Zhou （China Academy of Aerospace Aerodynamics）

AJCPP2018-136Study of the Influence of the Injection and Suction Flow Control Method on the Aerodynamic Performance of Supersonic Aircraft

Linjing Ma (Beijing Electro-Mechanical Engineering Institute)

AJCPP2018-094Numerical Analysis of Flow Characteristics of Blade Trailing Edge

Zheng Guanghua (Northwestern Polytechnical University)

AJCPP2018-041Performance Test of Korean Staged Combus-tion Cycle Engine

Chae-hyoung Kim (Korea Aerospace Research Institute)

AJCPP2018-112Analytic model and the influence of actuator number on the performance of Plasma Synthetic Jet Actuator Array

Zhibo ZHANG (Air Force Engineering University)

AJCPP2018-009A Plume Cross-Sectional Shape of Transverse Helium Injection Having Weakly Penetration into a Supersonic Boundary Layer by a Porous Injector

Yuya Nakatsuru (National Defense Academy of Japan)

AJCPP2018-096Application of Entropy Generation Theory to Flow Loss Analysis in Transonic Axial Compressors

WANG Wei (Huazhong University of Science and Technology)

AJCPP2018-050Experimental Investigation on the Liquid Film Generated by Slit Injector

Hyeongwon Lee (Seoul National University)

14:30-14:50

14:50-15:10

15:10-15:30

AJCPP2018-166Hybrid RANS/LES Simulation of Turbulent Combustion in a SCRAMJET Combustor using Level-Set Based Flamelet Model

Juyong Lee (Korea Aerospace University)

AJCPP2018-119Fluid-structure Interaction Simulation Study of Vibration Suppressing Effects of Axial Skewed Slots on Transonic Compressor Rotor

Ruoyang LIU (Aero Engine Academy of China)

AJCPP2018-099Design and Cold-flow Test of Bi-propellant Injectors for a Moon Exploration Thruster

Wongu Lee (Chungbuk National University)

AJCPP2018-062Enthalpy Estimation in a 0.4 MW Class Arc-Jet Plasma Wind tunnel

Rajesh Kumar Chinnaraj (Chonbuk National University)

AJCPP2018-164Improvement of compressible flamelet model using artificial neural network

Himeko Yamamoto (JAXA)

AJCPP2018-124Investigation of plasma synthetic jet actuators in quiescent flow

Mengxiao Tang (Air Force Engineering University)

AJCPP2018-106Effect of static deflection on a centrifugal compressor with backside cavity

Yurun Li (Xi’an Jiaotong University)

AJCPP2018-066Experimental Study of Plume Gas Tempera-ture Distribution and Infrared Signal in Micro Turbojet Engine

Sunmi Kim (Chonbuk National University)

AJCPP2018-126Investigation on the Large-scale simulation of multi-stage compressor

WangZiwei (China Aerodynamics Research and Development Center)

AJCPP2018-082Numerical Study of the Flow and Heat Transfer Characteristics of SupercriticalNitrogen in Roughened Straight Cooling Passage of Hypersonic Engines

Jiangnan Zhu (Aero Engine Academy of China)

AJCPP2018-115Control of the compressor tip leakage flow with plasma actuation

Zhang Haideng (Air force Engineering University)

AJCPP2018-069Combustion Tests of Clustered Hybrid Rocket Motors for Vertical Landing Application

Suhan Ko (Korea Aerospace University)

15:50-16:10

AJCPP2018-132Research of modeling and simulation on scramjet fuel supply system based on controllable cavitating Venturi

Siyu Wen (National University of Defense Technology)

AJCPP2018-071On the Development of Designing Method of Liquid-Propellant Rocket Propulsion System using Big Data

Hyoungkyung Mun (Korea Aerospace Research Institude)

AJCPP2018-118Flame Instability of Transverse Ethylene Injection in a Rectangular Supersonic Combustor with Symmetric Expansion

Guiyun Gao (National University of Defense Technology)

AJCPP2018-102Experimental Investigation of the Response of Methane Flames to the Acoustic Excitation

Yongchao Sun (National University of Defense Technology)

16:10-16:30

AJCPP2018-143Tomography for two-dimensional gas temperature distribution based on TDLAS

Can Luo (Xiamen University)

AJCPP2018-167Ignition Assist of Unheated Liquid Hydrocar-bon in a Supersonic Flowwith Atomization and Pilot Hydrogen

Inyoung Yang (Korea Aerospace Research Institute)

AJCPP2018-123Investigation of Infrared Signature of Serpentine Nozzle for Turbofan

Wen Cheng (Northwestern Polytechnical University)

AJCPP2018-154Schlieren Imaging of Underexpanded Jet Flow under Thermoacoustic Resonance

Seonghyeon Seo (Hanbat National University)

16:30-16:50

AJCPP2018-148Numerical Study on Effects of Injection Position on Supersonic Combustion of kerosene

Xiaojun Zhu (China Academy of Aerospace Aerodynamics)

AJCPP2018-010Study on Ignition Delay Time of Methane/Ethylene/Heptane Mixture Gas Using Chemical Reaction Analysis

Shinichiro Ogawa1 (Tohoku University)

AJCPP2018-127Loss Mechanism of the Tip Leakage Flow in a Low Speed Axial Compressor

Zhiyuan Li (Chinese Academy of Sciences)

AJCPP2018-156Experimental Study of Broadband Noise Generated from Linear Cascade

Yuji Koike (The University of Tokyo)

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GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

Break15:30-15:50GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall

C-5 Propulsion & Power componentsSession A-5 Computational Methods B-5 Fundamentals D-5 Test and Evalution

16:50-17:10

17:10-17:30

17:10-17:30

AJCPP2018-155Unsteady Flow Characteristics in The Entrance Section of a 2-D Mixed-compression Supersonic Inlet

Bing Wan (Hypervelocity Aerodynamics Institute of CARDC)

AJCPP2018-002Study of Axial Flow Turbine 1D Optimum Design

Jiang Zhuyu (China Aerodynamics Research and Development Center)

AJCPP2018-140The Design and Analysis of a New Type of Cooling Cycle for Scramjet

Bang-Yun Wang (National University of Defense Technology)

AJCPP2018-158Laser Optical Measurement of Acoustic Phenomena of a Supersonic Jet Using 2-D Position Sensitive Detector

Kazuya FUKATSU (The University of Tokyo)

AJCPP2018-157A Hybrid Particle-Fluid Simulation with Electron Inertia in a Hall Effect Thruster

Zhexu Wang (The University of Tokyo)

AJCPP2018-007Study on Effect of Cathode Position on SBS System Operation by Plume Diagnostics

Muhammad Safwatullah (Gifu University)

AJCPP2018-146Study on the Aerodynamics Performance of a Dual-Bell Nozzle

Kexin Wu (Andong National University)

AJCPP2018-018Improvement of Plasma Distribution by Propellant Injection Position in Miniature Microwave Discharge Water Ion Thrusters

Kengo Nakamura (Yokohama National University)

AJCPP2018-075A Conservative Overset Grid Method for Numerical Simulation of Propeller Slipstream

Cui Pengcheng (China Aerodynamics Research and Development Center Computa-tional Aerodynamics Institute)

AJCPP2018-097Aerodynamic Performance Study of Bionic Blade Inspired by the Seagull Wing Using Fluid-structure Interaction method

Fujia Hu（Xi’an Jiaotong University）

AJCPP2018-147Influence of the ambient pressure on the characterization of shock waves in the scramjet isolator

Yuan Ji (Shanghai Jiao Tong University)

AJCPP2018-163A ground combustion test facility for high altitude simulation

I.S. Yu (Chungnam National University)

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GuangYi Meeting Room QiongLin Meeting Room LiQuan 1 Multi-function Hall LiQuan 2 Multi-function Hall