7th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2015)

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1 7th Asia-Pacific International Symposium on Aerospace Technology (APISAT 2015) Cairns, Australia November 2015 ISBN:

2 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY Some format issues inherent in the e-media version may also appear in this print version. Copyright (2015) by Engineers Australia All rights reserved. Printed by Curran Associates, Inc. (2016) For permission requests, please contact Engineers Australia at the address below. Engineers Australia Engineering House 11 National Circuit Barton ACT 2600 Australia Phone: Fax: (02) Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY USA Phone: Fax: Web:

3 TABLE OF CONTENTS THE SIMULATION OF REFUELING DROGUE MOVEMENT AT DIFFERENT REFUELING DOCKING VELOCITIES... 1 L. Chen, X. Liu EXPERIMENTAL STUDY ON MECHANICAL CHARACTERISTICS OF ORNITHOPTER WING H. Endo, H. Fujii RESEARCH ON COHERENCE OF UNSTEADY FLOW OF MULTI-ELEMENT AIRFOIL Y. Jiao, N. Xiong NUMERICAL SIMULATION OF ROUGHNESS-INDUCED BOUNDARY LAYER TRANSITION H. Li, Y. Zheng WHIRL FLUTTER AND ROTOR HUB CENTER'S MOTION IMAGE OF TILTROTOR AIRCRAFT Z. Li, P. Xia PROGRESSIVE FAILURE ANALYSIS FOR LOW-VELOCITY IMPACT OF COMPOSITE SANDWICH PLATES BASED ON LAYERWISE/SOLID-ELEMENTS (LW/SE) METHOD D. Li, Y. Liu, X. Zhang DESIGN FOR FAULT TOLERANT PERMANENT MAGNET MOTOR CONTROL SYSTEM Z. Hao, S. Yu SERIES HYBRID-ELECTRIC PROPULSION FOR FIXED-WING VTOL UAV J. Bak, S. Cho, K. Park, S. Won, G. Lee, L. Cho, C. Moon, J. Cho A FINITE VOLUME METHOD FOR FULL-POTENTIAL EQUATION ON ADAPTIVE CARTERSIAN GRIDS F. Lv, X. Yu, T. Xiao CALCULATION STUDY OF HEAT GENERATION IN COUNTER-ROTATING CYLINDRICAL ROLLER BEARING P. Zhu, Z. Liu, W. Gao, J. Zhao, Y. Lu AEROSPACE DESIGN - A NEW WORLD THANKS TO DIGITAL TECHNOLOGY J. Page, J. Olsen COMPUTATION AND ANALYSIS OF LATERAL-DIRECTIONAL DYNAMIC DERIVATIVES OF THE NEAR SPACE SOLAR POWERED AIRCRAFT C. Ye, F. Li, G. Li DEVELOPMENT OF HARDWARE-IN-THE-LOOP SIMULATOR FOR EXPERIMENTAL WINGED ROCKET K. Shirakata, K. Yonemoto, H. Yamasaki, Y. Ura, H. Minote, A. Shiihara, S. Ohmori, S. Ishimoto, T. Mugitani THE STABILITY STUDY OF THE CONSTANT TEMPERATURE HOT-WIRE ANEMOMETER CONTROL CIRCUIT T. Zhang, H. Chen, Q. Wei, H. Jin THE PERFORMANCE STUDY OF AXIAL BREATHER WITH HONEYCOMB IN THE AERO- ENGINE LUBRICATION SYSTEMS J. Zhao, Z. Liu, P. Zhu, Y. Lu, G. Ren THE RESEARCH ON THE REAL-TIME AND FULL-ENVELOPED MODEL IDENTIFICATION OF TURBOFAN ENGINE S HYDRO-MECHANICAL ACTUATOR H. Xiao, W. Li, H. Li A FLUTTER BOUNDARY PREDICTION TECHNIQUE UNDER ATMOSPHERIC TURBULENCE EXCITATION Y. Li, L. Zhou, B. Yang NUMERICAL SIMULATION OF REBOUND CHARACTERISTICS OF SAND PARTICLES IMPACTING ON METAL PLATE J. Fan, T. Wu THE RESEARCH OF AEROSTAT GROUND TEST BASED ON ROCKET SLED TECHNIQUES S. Huang, J. Liu, S. Huang, J. Liu RESEARCH ON ATMOSPHERIC ENTRY PILL FOR THE UPPER ATMOSPHERE OBSERVATION K. Sakuyama, H. Sahara, M. Watanabe INVESTIGATION ON INFLUENCE OF BRAID ANGLE AND BOUNDARY CONDITION FOR IMPACT RESPONSE OF TRIAXIAL BRAIDED COMPOSITES WITH SUBCELL MODEL USING SOLID ELEMENTS H. Tan, L. Liu, Y. Guan, W. Chen, Z. Zhao

4 MATCHING CALCULATION AND PERFORMANCE ANALYSIS FOR AERO-ENGINE STARTING AIR FEEDING SYSTEM X. Huang, X. Zhao EFFECT OF ROTATIONAL DIRECTION OF TRIPLE-SWIRLER ON COLD FLOW CHARACTERISTICS X. He, Z. Zhao DEVELOPMENT OF A DYNAMIC PROPULSION MODEL FOR ELECTRIC UAVS A. Gong, D. Verstraete AIR COMBAT TACTICAL DECISION UNIT BASED ON FINITE STATE MACHINE H. Song, L. Xia, C. Shang, H. Zhan A METHOD OF MONOCULAR VISION BASED ASYNCHRONOUS ELEVATION MEASUREMENT FOR MUAV P. Wen, Y. Cheng, Y. Zhang, Y. Li AERODYNAMIC CHARACTERISTICS OF A DEPLOYABLE-WING AIRPLANE WITH AN ELEVON FOR MARS EXPLORATION G. Yamada, A. Miyazaki, H. Kawazoe AERODYNAMIC PARAMETERS ESTIMATION FOR REENTRY CAPSULE G. Wang, Z. Liu, Z. Liu, Y. Zhou RESEARCH AND VALIDATION OF GLOBAL SKIN FRICTION MEASUREMENT TECHNIQUES BASED ON FLUORESCENT OIL FILM Z. Huang, H. Wang, L. Wei ANALYSIS OF LOW SPEED STABILITY DERIVATIVES OF A HYPERSONIC TEST VEHICLE J. Leyaratnam, D. Verstraete PARAMETER OPTIMIZATION OF MULTISTAGE MISSILE FOR TERMINAL VELOCITY MAXIMIZATION J. Lee, S. Hong, Y. Kim, M. Tahk RESPONSE TIME ANALYSIS OF TTCAN BUS FOR AERO-ENGINE DISTRIBUTED CONTROL SYSTEM X. Fan, M. Pan, J. Huang NETWORK-BASED GUARANTEED COST TRACKING CONTROL FOR AERO-ENGINE R. Zhang, M. Pan, J. Huang ASSESSMENT OF NUMERICAL SIMULATION FOR UNDEREXPANDED SONIC JET ISSUED FROM AXISYMMETRIC CONVERGENT NOZZLES Y. Akita, S. Nakao, D. Ono, Y. Miyanto A STUDY ON AERODYNAMIC CHARACTERISTICS OF AIRCRAFT MODEL WITH VORTEX GENERATORS BY WAKE MEASUREMENTS M. Kashitani, Y. Yamaguhi, K. Kusunose, Y. Takita THE CHANGING SIZE OF THE COMMERCIAL AVIATION PASSENGER AND ITS POTENTIAL IMPACT ON THE AVIATION INDUSTRY D. Melis, J. Silva, R. Clothier EXPERIMENTAL ANALYSIS OF THE DYNAMIC CHARACTERISTICS OF AN ORNITHOPTER M. Kamii, H. Okubo, H. Fujii, H. Endo TESTS OF ALTERNATIVE FUEL BLENDS IN MICRO-TURBOJET ENGINES J. Vivian, A. Seeber, G. Dorrington RESEARCH ON THE TECHNOLOGY OF TURBOFAN ENGINE STARTING FAULT DIAGNOSIS Z. Tang, W. Zhou, J. Huang, Q. Zhang STUDY ON A MORPHING WING STRUCTURE USING OPEN-SECTION MEMBER A. Aso, H. Tanaka RESEARCH ON FIXED WING UAV FORCED LANDING TECHNOLOGY G. Yang, K. Song, X. Zhu, W. Wei RESEARCH TO IDENTIFY MATHEMATICAL MODELS OF QUADROTOR N. Dung, T. Hung AERODYNAMIC ANALYSIS OF AIRBORNE MAGNETIC GRADIENT MEASUREMENT APPLIED ON HIGH ASPECT RATIO-UAV Y. Fu, C. Jun, S. Tian CALCULATING DYNAMICS OF THE DAMPER SYSTEM FOR RECOVERING THE PAYLOAD IN A MODEL CARRIER ROCKET N. Dung, T. Hung

5 FLOW VISUALIZATION OF SEPARATION ON A SHROUDED ROTOR INLET IN A CROSSWIND H. Otsuka, K. Nagatani RECENT DEVELOPMENTS OF EXPERIMENTAL WINGED ROCKET: AUTONOMOUS GUIDANCE AND CONTROL DEMONSTRATION BY FLIGHT TEST T. Ohki, K. Yonemoto, M. Yamamoto, H. Yamazaki, M. Ichige, G. Surendra, S. Ishimoto, T. Mugitani AERODYNAMIC SHAPE OPTIMIZATION OF A BLENDED WING BODY AIRCRAFT WITH DISTRIBUTED PROPULSION SYSTEM W. Yan, J. Wu AN EXPLORATION OF SURFACE INTEGRITY REMANUFACTURING FOR AEROENGINE COMPONENTS X. Qian, H. Yong, T. Hou NAUTICAL TECHNOLOGY FOR AIRCRAFT EMERGENCY LOCATION TRACKING IN A MARITIME ENVIRONMENT L. Peters, C. Bil, P. Marazocca HYDRODYNAMIC RAM BEHAVIOUR IN RAM SIMULATOR H. Bae, K. Woo, I. Kim, J. Kim INTEGRATING PAIRWISE PROXIMITY-BASED AIR TRAFFIC CONTROL DIFFICULTY INDICES INTO AN AIRSPACE INDEX N/A THE VERIFICATION AND EXPERIMENT RESEARCH ON OPTICAL FLOW H. Wang, L. Wei, Z. Huang INTERMITTENT FAILURE DETECTION OF AVIATION ELECTRICAL CONNECTORS Z. Cai, S. Zhang EXPERIMENTS ON BUOYANCY AND CONDENSATION HEAT TRANSFER OF HELIUM OR AIR AND STEAM MIXTURES SUPPORTING VENUS AEROSTAT STUDY A. Herbert THE NOISE CREATED BY AN AIRFOIL IN THE WAKE OF A SUBBOUNDARY LAYER STEP D. Moreau, C. Doolan FLOW ANALYSIS OF THE EFFECT OF TUBE GEOMETRY ON THE PERFORMANCE OF PRE-COOLERS FOR TURBINE-BASED HYPERSONIC AIR-BREATHING PROPULSION T. Jones, N. Karwa, H. Ogawa, G. Rosengarten ERROR ANALYSIS WITH THE TRADITIONAL NUMERICAL METHOD OF THE LATERAL JET INTERACTION FOR THE SUPERSONIC FLOW L. Yang, Z. Ye LOAD INSTRUCTION STRATEGY OF DYNAMOMETER FOR STARTING PROCESS OF GAS TURBINE STARTERS X. Zhao, X. Huang INVESTIGATION OF STOCHASTIC SIMULATION INTO HELICOPTER STRUCTURAL CRASH AFTER AUTOROTATION SCENARIOS Y. Pei, J. Page, G. Pearce AIR TRAFFIC OPEN DATA AND ITS IMPROVEMENT Y. Fukuda, M. Oka, N. Wickramasinghe, K. Uejima A NUMERICAL RESEARCH ON AERODYNAMIC INTERFERENCE OF DIAMOND-WING SENSOR-CRAFT Z. Wang, X. Zhu, Z. Zhou, C. Zhang, Y. Wang LIMIT TESTING OF A FOAMED CONCRETE ARRESTOR'S RESISTANCE TO JET BLAST X. Xiao, Y. Shi, H. Yao VIBRO-ACOUSTIC COUPLING RESPONSE ANALYSIS AND NOISE CONTROL OF THE WINDOW AND CABIN OF AIRCRAFT BY APPLYING ACOUSTIC WAVEGUIDE MODAL EXPANSION METHOD S. Ning, Z. Shi, J. Zhang, D. Qian, J. Li SIMULATION RESULTS OF COOPERATIVE FORMATION FLYING CONTROL OF UAVS WITH COLLISION AVOIDANCE BASED ON ORCA A. Mello, R. Chiaramonte, L. Filho, R. Inoue, K. Branco CONVERGENCE TECHNOLOGY R&D FOR AIRCRAFT DESIGN WITH RESPECT TO AVIATION SAFETY AND GREEN AVIATION/AIRCRAFT S. Nah ACCURACY OF ONE-DIMENSIONAL HEAT TRANSFER MODEL OF RADIOISOTOPE THERMOELECTRIC GENERATOR J. Kim, J. Park, J. Hong, G. Son

6 A CASE STUDY FOR IMPROVING AIRCRAFT DEVELOPMENT PROJECTS: HOW DO STUDENTS MANAGE A TEAM UNDER THE CURRICULUM? J. Kumura, S. Suzuki DUAL FIELD ANALYSIS OF POLING DESIGN OF PVDF FIBRES FOR ENERGY HARVESTING APPLICATIONS S. Waqar, S. John, I. Khan, C. Wang, A. Ladigus-Grange, L. Wang, F. Coman A COMPUTATIONAL STUDY ON TAIL BUFFETING SUPPRESSION BY AN INFLATABLE BUMP Q. Zhang, Z. Ye UAV RECHARGING USING NON-CONTACT WIRELESS POWER TRANSFER M. Simic, C. Bil, V. Vojisavljevic, J. Perilla AN INTEGRATED DESIGN OF LIGHT-WEIGHT GRADED STRUCTURE FOR HYPERSONIC VEHICLES Q. Lu, H. Han, L. Hu, J. Yu INVESTIGATION OF DIVERT CONTROL JET INTERACTION EFFECTS ON AERODYNAMIC CHARACTERISTICS J. Fu, Y. Liu, Z. Ni, N. Cao STUDY OF GROUND TEST METHOD FOR NEAR SPACE PROPELLER X. Li, G. Li, B. Zhou, W. Zhu, K. Sun ANALYSIS AND SIMULATION OF FC-1553B DOUBLE-STAR NETWORK IN AVIONICS SYSTEM X. Zhu, H. Zhou, F. Zhang, X. Yang APPLICATION OF AEKF PARAMETER IDENTIFICATION TO UAV AUTOPILOT Z. Liu, G. Wang, Y. Zhou A PROBABILISTIC APPROACH TO AIRCRAFT ARRIVAL SEQUENCING AND CONFLICT RESOLUTION Y. Matsuno, T. Tsuchiya IN-PLANE MECHANICAL PROPERTIES OF INTEGRATED SKINS L. Chang, X. Shen, J. Wang A COMPARATIVE STUDY OF ROAD EXTRACTION TECHNIQUES FROM AERIAL IMAGERY A NAVIGATIONAL PERSPECTIVE A. Volkova, P. Gibbens UNSTEADY QUASI-ONE-DIMENSIONAL MODELLING FOR PROPULSION SYSTEMS C. Doolan Author Index

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