NUMERICAL STUDY ON EFFECT OF OPERATING TABLE PROTECTED BY HORIZONTAL LAMINAR FLOW SCREEN
Fan Juli;Yang Xiaojing;Wang Sihan;Zheng Xiaoyi;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:292-296

HYBRID CARTESIAN GRID/GRIDLESS METHOD FOR CALCULATING VISCOUS FLOWS OVER MULTI-ELEMENT AIRFOILS
Pu Saihu;Chen Hongquan;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:232-236

ADAPTIVE HYBRID CARTESIAN GRID METHOD FOR VORTEX-DOMINATED FLOWS
Hu Ou;Zhao Ning;Liu Jianming;Wu Jie;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Department of Mathematics;Xuzhou Normal University;

..............page:221-226

3D NUMERICAL SOLUTION OF AERO-NOISE WITH HIGH-ORDER DISCONTINUOUS GALERKIN METHOD
L Hongqiang;Sun Qiang;Qin Wanglong;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:227-231

CALCULATING METHOD OF AERODYNAMIC HEATING FOR HYPERSONIC AIRCRAFTS
Ji Weidong;Wang Jiangfeng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:237-242

MULTIGRID TECHNIQUE APPLIED TO LINEAR TIME-DEPENDENT HYPERBOLIC SYSTEMS
Naren Deore;Avijit Chatterjee;Pimpri Chinchwad College of Engineering;Department of Aerospace Engineering;India Institution of Technology;

..............page:243-247

MODAL DISCONTINUOUS GALERKIN METHOD FOR SHOCK WAVE STRUCTURES
Nam Tuan Phuong Le;Rho Shin Myong;Department of Aerospace and System Engineering and Research Center for Aircraft Parts Technology;Gyeongsang National University;

..............page:252-256

LONG-TERM RIGOROUS NUMERICAL INTEGRATION OF NAVIER-STOKES EQUATION BY NEWTON-GMRES ITERATION
JuliusRhoanT.Lustro;Lennaert van Veen;Genta Kawahara;College of Engineering and Agro-Industrial Technology;University of the Philippines Los Banos;Faculty of Science;University of Ontario Institute of Technology;Department of Mechanical Science and Bioengineering;Osaka University;1-3 Machikaneyama;

..............page:248-251

FAST SIMULATION OF FLOWS IN SHOCK TUBE WITH AREA CHANGE
Zhu Hao;Shen Qing;Gong Jian;China Academy of Aerospace Aerodynamics;

..............page:260-263

NUMERICAL AND EXPERIMENTAL STUDY OF LURE MOVING IN WATER
Wataru Sekiguchi;Naoya Takahashi;Shigeho Noda;Ryutaro Himeno;Graduate School of Engineering;Tokyo Denki University;Department of Engineering;Tokyo Denki University;Advanced Center for Computing and Communication;

..............page:257-259

PARAMETER ANALYSIS ON CIRCULATION CONTROLLED CIRCULAR CYLINDER FOR NOTAR~TM TAIL BOOM
Li Jiachun;Yang Weidong;Gao Ning;National Key Laboratory of Rotorcraft Aeromechanics;Nanjing University of Aeronautics and Astronautics;Institute of Unmanned Aerial Vehicle;Nanjing University of Aeronautics and Astronautics;

..............page:282-291

SOUND GENERATION AND INTERACTIONS OF SHOCK WAVES WITH ROWS OF VORTICES
Xu Dongyang;Guan Hui;Wu Chuijie;State Key Laboratory of Structural Analysis for Industrial Equipment;Dalian University of Technology;School of Aeronautics and Astronautics;Dalian University of Technology;Department of Mathematics &Physics;PLA University of Science and Technology;

..............page:276-281

EFFECT OF CONTACT ANGLE HYSTERESIS ON DROPLET BEHAVIORS:TWO-PHASE LATTICE BOLTZMANN SIMULATION
Wang Lei;Xu Changyue;Department of Modern Mechanics;University of Science and Technology of China;College of Aerospace Engineering;Nanjing University of Aeronautics andAstronautics;

..............page:270-275

APPLICATION OF CFD TECHNOLOGY IN WIND TURBINE ICING PROBER DESIGN
Yi Xian;Chen Kun;Wang Kaichun;Ma Honglin;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;

..............page:264-269