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ACCEPTED PAPERS - CATEGORY B – STANDBY These papers are standby for oral presentations in case papers are withdrawn from an appropriate session Full papers will appear in the congress CD-Rom Proceedings They may also be presented as posters in the Poster area |
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1. AIRCRAFT AND SYSTEMS INTEGRATION :
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ICAS2012-1.1ST: J. -L. Hernando, R. Martínez-Val: Univ. Politécnica de Madrid, Spain |
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ICAS2012-1.4ST: T. Lwin, N. A. Vu, K. Jimin, et al: Konkuk Univ., Korea AN INTEGRATED FRAMEWORK FOR INNOVATIVE COMPOUND GYROPLANE DESIGN SYSTEM |
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ICAS2012-1.7ST: A. M. Abdalla, F. M. Catalano, P. C. Greco, et al: Univ. of São Paulo, Brazil THE INFLUENCE OF DEMOISELLE AIRCRAFT ON LIGHT AND GENERAL AVIATION DESIGN |
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ICAS2012-1.8ST: L. B. Gutierrez, O. Hazbon, B. Appel*: Univ. Pontificia Bolivariana, Colombia; *TU Berlin, Germany UAS DESIGN REQUIREMENTS FOR OPERATION IN COLOMBIAN MOUNTAIN ENVIRONMENTS |
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ICAS2012-1.9ST: P. O. Jemitola, J. P. Fielding: Cranfield Univ., UK |
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ICAS2012-1.10ST: K. -S. Zhang, P. -B. Ji, A. Bakar, et al: NWPU, Xi'an, China MULTIDISCIPLINARY EVALUATION OF TRUSS-BRACED WING FOR FUTURE GREEN AIRCRAFT |
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2. AERODYNAMICS : |
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ICAS2012-2.2ST: J. -H. Kim, K. -H. Kim, A. Jon*: Seoul National Univ., Korea; *Sejong Univ., Korea |
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ICAS2012-2.3ST: R. F. Xu, R. Z. Qian, W. Lei: AVIC, The First Aircraft Inst., Xi'an, China MULTI-OBJECTIVE AERODYNAMIC OPTIMIZATION DESIGN OF MULTI-ELEMENT AIRFOIL USING KRIGING MODEL |
ICAS2012-2.11ST: A. Hashimoto, K. Murakami, T. Aoyama, et al: JAXA, Japan |
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ICAS2012-3.1ST1: G. Liu, Z. Li, M. Tang: AVIC Aero. Res. Inst., Harbin, China CHARACTERISTICS OF AN 80-DEG SWEPT DELTA WING IN WING ROCK OR FREE YAWING |
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ICAS2012-3.1ST2: K. Asai, A. Konno, X. Jiang, et al: Tohoku Univ., Japan MULTI-DEGREE-OF-FREEDOM DYNAMIC WIND-TUNNEL TESTING OF A DELTA WING USING A ROBOTIC MANIPULATOR |
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ICAS2012-3.6ST: D. Mateescu, O. Scholz, C. Wang: McGill Univ., Canada STEADY AND UNSTEADY FLOWS PAST AIRFOILS AT LOW REYNOLDS NUMBERS IN THE PROXIMITY OF THE GROUND |
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ICAS2012-3.8ST: T.-H. Nguyen-Bui, J. Dubois: CEA / CESTA, France |
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ICAS2012-9.5ST: J. Bayandor, A. Kurdila: Virginia Tech, USA A LEAP IN LEARNED BIO-INSPIRED FLIGHT |
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ICAS2012-9.8ST: T. Wan: Tamkang Univ., Taiwan, China AERODYNAMIC ANALYSIS OF 3-D FLAPPING WING MOTION VIA THE HILBERT-HUANG TRANSFORM METHOD |
ICAS2012-9.11ST1: A. Fisher, S. Watkins, J. Watmuff: RMIT Univ., Australia DYNAMIC SURFACE PRESSURE MEASUREMENTS ON A FLAPPING WING IN SMOOTH AND TURBULENT FLOW |
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ICAS2012-10.6ST1: Z. Patek, J. Cervinka, P. Vrchota: VZLU, Prague, Czech Republic |
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ICAS2012-10.6ST2: G. A. Vio, D. S. Stanley: Univ. of Sydney, Australia |
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ICAS2012-11.4ST: X. Zhang, Z. Gao, B. Zhong*: NWPU, Xi'an, China; *COMAC, China EXTENSIONS OF MENTER’S SST TRANSITION MODEL TO SIMULATE HYPERSONIC AND CROSS-FLOW TRANSITION |
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ICAS2012-11.10ST: J. Liu, Z. H. Han, W. P. Song: NWPU, Xi'an, China COMPARISON OF INFILL SAMPLING CRITERIA IN KRIGING-BASED AERODYNAMIC OPTIMIZATION |
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3. MATERIALS AND STRUCTURES : |
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ICAS2012-7.1ST: B. G. Falzon, A. Faggiani, D. Brunner*: Monash Univ., Australia; *ETH Swiss Federal Inst. of Technology, Switzerland LAY-UP OPTIMIZATION OF COMPOSITE PLATES TO DELAY MODE-JUMP INSTABILITIES |
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ICAS2012-7.3ST: H. -F. Qi, D. -B. Liu, F. -L. Sun: BIAM, Beijing, China |
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ICAS2012-7.5ST: M. Malis, T. Urik, O. Uher*: Brno Univ. of Technology, Czech Republic; *Compotech Plus s.r.o., Czech Republic THE CFRP SAILPLANE WING SEGMENTS MANUFACTURED BY FILAMENT PLACEMENT |
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ICAS2012-7.7ST: X. Zheng, T. Qu, Z. Shen*: NWPU, Xi'an, China; *Aircraft Strength Research Inst. of China, China ON THE KNEE-POINT PHENOMENON IN COMPOSITE LAMINATES UNDER LOW-VELOCITY IMPACT AND QUASI-STATIC INDENTATION |
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ICAS2012-7.9ST: M. Palizvan, S. M. Mohseni Shakib: Imam Hossein Univ., Iran POST-BUCKLING BEHAVIOR AND PROPAGATION OF DELAMINATION FOR COMPOSITE PANELS IN DIFFERENT DELAMINATION SIZES |
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ICAS2012-8.1ST: T. Hou, G. Pearce*, B. G. Prusty*, et al: UNSW / CRC-ACS, Australia; *UNSW, Australia |
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ICAS2012-8.2ST: A. Pistek: Inst. of Aerospace Eng., Brno Univ. of Technology, Czech Republic ANALYTICAL METHOD FOR LIMIT LOAD CAPACITY CALCULATION OF THIN WALLED AIRCRAFT STRUCTURES |
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ICAS2012-8.4ST: V. A. Bespalov, T. B. Gotseluk*, V. Chaplygin: FSUE, Russian Federation; *FSUE & Novosibirsk State Technical Univ., Russian Federation COMPUTATIONAL AND EXPERIMENTAL RESEARCH OF BOLT JOINTS OF METAL AND COMPOSITE IN AIRFRAMES |
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ICAS2012-8.10ST: J. Vine, X. Yu: DSTO, Australia |
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4. PROPULSION : |
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ICAS2012-4.2ST: Y. H. He, C. K Liu: BIAM, China ENGINEERING FAILURE MODES AND FRACTURE CHARACTERISTICS OF SINGLE CRYSTAL SUPERALLOY BLADES |
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ICAS2012-4.3ST: S. Hassan, M. Coporrella, M. Robertson, et al: KTH, Sweden EFFECT ON THE AERODYNAMIC FORCING IN AN AXIAL TURBINE STAGE ON VARYING STATOR BLADE SHAPE |
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ICAS2012-4.4ST: X. Yu, H. Y. Lu*, J. N. Sun**, et al: Shenyang Aeroengine Research Inst. & BUAA, China; *Shenyang Aeroengine Research Inst., China; **BUAA, China STUDY OF THE PRESSURE DROP FOR RADIAL INFLOW BETWEEN CO-ROTATING DISCS |
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ICAS2012-4.6ST1: N. Arai, K. Hiraoka: Tokai Univ., Japan COMPARISON OF PERFORMANCE OF PROPELLER BLADES BY DIFFERENCE IN PLANAR SHAPE |
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ICAS2012-4.6ST2: H. Djojodihardjo, M. F. A. Hamid: Putra Univ., Malaysia COMPUTATIONAL STUDY ON THE INFLUENCE OF COANDA JET ON AIRFOILS: TWO-DIMENSIONAL CASE |
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5. FLIGHT DYNAMICS AND CONTROL : |
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ICAS2012-5.9ST: S. W. Yan, Z. H. Gao: NWPU, Xi'an, China STUDY ON MODELING PILOT BEHAVIOR BY ARTIFICIAL NEURAL NETWORK |
ICAS2012-5.10ST: X. W. Xu, W. Zhang: NWPU, Xi'an, China RESEARCH ON METHODS OF DYNAMIC MODELING AND SIMULATION FOR MORPHING WING AIRCRAFT |
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ICAS2012-11.9ST: W. Yuan, J. Katupitiya: UNSW, Australia |
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6. SYSTEMS, SUBSYSTEMS AND EQUIPMENT : |
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ICAS2012-6.5ST: F. Minaeifard, M. Mirzaei, A. Hamidiyanfar, et al: Aviation Industrial Center Univ. of Tehran, Iran AN OVERVIEW OF THE DEICING AND ANTIICING TECHNOLOGIES |
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ICAS2012-6.8ST: J. -C. Derrien: Sagem Defense Securite, France ELECTROMECHANICAL ACTUATOR (EMA) ADVANCED TECHNOLOGIES FOR FLIGHT CONTROLS |
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ICAS2012-6.11ST: P. J. Callus, K. J. Nicholson, A. Bojovschi*, et al: DSTO, Victoria, Australia; *RMIT Univ., Australia A PLANAR ANTENNA ARRAY MANUFACTURED FROM CARBON FIBRE REINFORCED PLASTIC |
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8. AIR TRANSPORT SYSTEM EFFICIENCY : |
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ICAS2012-10.1ST: D. Zammit-Mangion, S.A.H. Rydell*, R. Sabatini*, et al: Univ. of Malta, Malta, & Cranfield Univ.,UK; *Cranfield Univ., UK |
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9. SAFETY AND SECURITY : |
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ICAS2012-9.4ST: C. Cuerno, M. J. Guerrero, R. Arnaldo, et al: CIAIAC, Spain |
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ICAS2012-9.10ST: A. Tezuka, T. Nakamura, Y. Higashiyama, et al: Waseda Univ., Japan DEVELOPMENT OF LAPTOP PC TOOL WITH VISUAL PROJECTION FOR FLIGHT MANAGEMENT TRAINING |