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ACCEPTED PAPERS - CATEGORY C - POSTERS These papers will be presented in the Poster area Most papers will also appear in the Congress CD Proceedings |
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1. AIRCRAFT AND SYSTEMS INTEGRATION: |
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ICAS2012-P1.1: S. Winship, Northrop Grumman Corporation, USA FIRE-X 407 DEVELOPMENT: UNMANNING THE BELL HELICOPTER 407 WITH THE US NAVY FIRE SCOUT MQ-8B AUTONOMOUS SYSTEM |
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ICAS2012-P1.2: R. Zhang, D. Cui*, H. Du, et al, Beihang Univ. (BUAA), China; *AVIC, China THE METHOD FOR NONLINEAR ANALYSIS OPTIMIZATION IN AERONAUTICAL RESEARCH |
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ICAS2012-P1.3: G. Roberts, D. Langkamp, W. Crowther, Univ. of Manchester, UK TETHERING UNMANNED ROTORCRAFT FOR HIGH-ENDURANCE OPERATIONS |
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ICAS2012-P1.4: A. Nagy, J. Rohacs, Budapest Univ. of Technology and Economics, Hungary |
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2. AERODYNAMICS: |
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ICAS2012-P2.1: N. V. Voevodenko, A. A. Gubanov, TsAGI, Russian Federation NUMERICAL RESEARCH OF THE AIR INTAKE LOCATION INFLUENCE ONTO THE HIGH-SPEED AIRCRAFT PERFORMANCE |
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ICAS2012-P2.2: Z. B. Zhang, J. H. Sang, Chengdu Aircraft Research and Design Inst., China THE INTEGRATION OPTIMIZATION DESIGN OF AERODYNAMIC AND STEALTH FOR FIGHTERS |
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ICAS2012-P2.3: J. Chai, H. Che, The First Aircraft Inst. of AVIC, China TRANSONIC DRAG REDUCTION ON A SUPERCRITICAL WING SECTION USING SHOCK CONTROL BUMPS |
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ICAS2012-P2.4: K. Zhao, Z. -H. Gao, J. -T. Huang, NWPU, Xi'an, China |
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ICAS2012-P2.5: J. G. Yu, G. Z. Liu, M. Z. TangChina Aerodynamics Research Inst. of Aeronautics, China FLOW CONTROL TEST RESEARCH OF AIRCRAFT MODEL WITH ADJUSTABLE CANAEDS |
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ICAS2012-P2.6: S. M. Bosnyakov, A. R. Gorbushin, S. V. Mikhaylov, et al, TsAGI, Russian Federation AN EXPERIENCE OF USING NUMERICAL METHODS IN EXPERIMENTAL INVESTIGATIONS OF TsAGI |
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ICAS2012-P2.7: Z.. X. Xiao, Z. W. Duan, J. B. Huang, et al, Tsinghua Univ., China INVESTIGATION OF PASSIVE FLOW CONTROL METHODOLOGIES USING SST-IDDES |
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ICAS2012-P2.8: L. M. B. C. Campos, F. J. P. Lau, CCTAE, IST, Portugal ON SOUND GENERATION BY MOVING SURFACES AND CONVECTED SOURCES IN A FLOW |
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ICAS2012-P2.9: J. J. Zhang, G. Qian, J. Si, Shanghai Aircraft Design Research Inst., China THE STUDY ON THE AIRCRAFT INTEGRATED CHARACTERS WITH DIFFERENT HEIGHT WINGLETS |
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ICAS2012-P2.10: G. K. Vedeshkin, A. Dubovitskiy, D. Bondarenko*, et al, CIAM, Russian Federation; *EADS, Russian Federation EXPERIMENTAL INVESTIGATIONS OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT |
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ICAS2012-P2.11: R. Isozumi, K. Kubo, D. Ono, et al, Univ. of Kitakyushu, Japan |
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ICAS2012-P2.12: T. Atobe, JAXA, Japan STABILIZING EFFECT OF LONGITUDINAL-WALL OSCILLATION ON 2D CHANNEL FLOW |
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ICAS2012-P2.13: M. Martínez, C. Cuerno, Universidad Politécnica de Madrid, Spain PRELIMINARY AERODYNAMIC INVESTIGATION OF AN UNMANNED BOX-WING AIRCRAFT |
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ICAS2012-P2.14: Y. -F. Sun, S. -P. Yang, Shanghai Aircraft Design and Research Inst., COMAC, China A PRELIMINARY CFD INVESTIGATION ON REAR FUSELAGE SUPPORT CORRECTION |
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ICAS2012-P2.15: J. Lee, S. Joo*, Hoseo Univ., Korea; *EeGen Co., Korea |
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ICAS2012-P2.16: Y. Zhong, K. Zhao, Commercial Aircraft Corporation of China, China CFD-BASED RESEARCH OF STRAKE EFFECTS FOR LOW SPEED HIGH LIFT CONFIGURATION |
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ICAS2012-P2.17: S. P. Yang, COMAC, China ANALYSIS OF FLUCTUATING LOAD OF A CIRCULAR CYLINDER UNDER THE FUSELAGE |
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ICAS2012-P2.18: N. Mirkov, B. Rasuo, Univ. of Belgrade, Serbia MANEUVERABILITY OF AN UAV WITH COANDA EFFECT BASED LIFT PRODUCTION |
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ICAS2012-P2.19: T. Bortholin, F. M. Catalano, Univ. of São Paulo, Brazil COMPUTATIONAL INVESTIGATION OF ICING CONTAMINATION ON AIRFOIL |
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ICAS2012-P2.20: K. Fujita, Tohoku Univ., Japan EVALUATION OF DYNAMIC BEHAVIOR OF A DEPLOYABLE WING UAV BY DROP TEST |
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ICAS2012-P2.21: A. A. Ryzhov, V. G. Soudakov, TsAGI, Russian Federation ENERGY SUPPLY EFFECT ON SUPERSONIC BOUNDARY LAYER RECEPTIVITY AND STABILITY |
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ICAS2012-P2.22: J. Kurihara, Y. Inada, Tokai Univ., Japan |
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ICAS2012-P2.23: S. T. Kim, Y. Kim*, T. K. Reu, Agency for Defense Development, Korea; *Korean Air R&D Center, Korea CFD COMPUTATION OF THE GROUND EFFECT ON AIRPLANE WITH HIGH ASPECT RATIO WING |
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ICAS2012-P2.24: S. Zietarski, S. Kachel, A. Kozakiewicz, Military Univ. of Technology, Poland |
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3. MATERIALS AND STRUCTURES: |
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ICAS2012-P3.1: J. Cecrdle, O. Vich, VZLU, Prague, Czech Republic EIGENVALUE AND FLUTTER SENSITIVITY ANALYSIS OF AIRLINER WING |
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ICAS2012-P3.2: L. M. B. C. Campos, A. C. Marta, CCTAE, IST, Portugal |
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ICAS2012-P3.3: T. J. Harrison, RMIT Univ., Australia INTERGRANULAR CORROSION PROTOCOL DEVELOPMENT FOR 7075-T651 EXTRUSION |
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ICAS2012-P3.4: S. V. Neilson, A. C. Orifici, C. H. Wang, RMIT Univ., Australia INVESTIGATION INTO OPTIMISED COMPOSITE SCARF REPAIRS WITH PRACTICAL CONSTRAINTS |
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ICAS2012-P3.5: E. Unay, D. Gurak, V. Ozerciyes, et al, Turkish Aerospace Industries, Inc., Turkey |
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ICAS2012-P3.6: F. Mollaei, M. R. Moosavi, A. Abedian, et al, Sharif Univ. of Techn., Iran FINDING TUNING FREQUENCY OF SYMMETRIC AND ANTI-SYMMETRIC LAMB WAVES USING FEM |
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ICAS2012-P3.7: M. Palizvan, S. M. Mohseni Shakib, Imam Hossein Univ., Iran BUCKLING AND POST-BUCKLING RESPONSES OF SQUARE LAMINATE WITH VARIOUS SHAPED CUTOUTS UNDER DIFFERENT LOADINGS |
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ICAS2012-P3.8: Z. Soltani, M. Ekhtiari, A. AbedianSharif Univ. of Technology, Iran |
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ICAS2012-P3.9: K. -J. Lee, H. -U. Oh, M. -S. Jo*, et al, Agency for Defence Development, Korea; *Samsung Tales, Korea |
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4. PROPULSION: |
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ICAS2012-P4.1: Z. B. Zhang, J. H. SangChengdu Aircraft Research and Design Inst., China EXPERIMENTAL INVESTIGATION OF INFRARED STEALTH TECHNOLOGIES OF AERO-ENGINE EXHAUST SYSTEM |
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ICAS2012-P4.2: Y. Xu, Chinese Aeronautical Establishment, China JET NOISE REDUCTION BY MICROJETS |
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ICAS2012-P4.3: A. Chevagin, TsAGI, Russian Federation INTAKE CAPABILITY IMPROVEMENTS IN RAMJET-TYPE PROPULSION SYSTEM |
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ICAS2012-P4.4: C. -H. Kim, I. -S. Jeung*, B. Choi**, et al, Defense Agency for Technology and Quality, Korea; *Seoul National Univ., Korea; **Tohoku Univ., Japan EFFECT OF VENT MIXER TO MIXING CHARACTERISTICS IN SUPERSONIC FLOW |
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ICAS2012-P4.5: N. Tanaka, T. Mizukaki, Tokai Univ., Japan VISUALIZATION OF UNSTEADY BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL |
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ICAS2012-P4.6: H. J. Nam, J. W. Kim, O. J. Kwon, KAIST, Korea MODELING OF NO AND OH INFRARED RADIATION ON A CONVERGENT-DIVERGENT NOZZLE |
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ICAS2012-P4.7: C. K. Liu, B. Zhang, C. H. Tao, Beijing Inst. of Aeronautical Materials, China FRACTURE ANALYSIS OF BLADE DOVETAIL OF TC11 TITANIUM ALLOY |
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ICAS2012-P4.8: J. J. Foenander, RMIT Univ., Australia DESIGN OF A TWO-DIMENSIONAL GASDYNAMIC NOZZLE USING MULTI-OBJECTIVE PARTICLE SWARM OPTIMISATION |
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ICAS2012-P4.9: J. Song, J. J. Yi, T. H. Kim, et al Yonsei Univ., Korea THERMAL ANALYSIS NEAR SECONDARY INJECTION HOLE IN SITVC SYSTEM |
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ICAS2012-P4.10: F. A. Slobodkina, V. V. Malinin, A. I. Tarasov*, CIAM, Russian Federation; *Lulka RDC, Russian Federation |
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ICAS2012-P4.11: M. Attia, J. Hou, DSTO, Australia |
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ICAS2012-P4.12: A. Che Idris, M. R. Saad, H. Zare-Behtash, et al, Univ. of Manchester, UK PERFORMANCE ANALYSIS OF A SCRAMJET INLET-ISOLATOR USING EXPERIMENTAL & NUMERICAL METHODS |
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ICAS2012-P4.13: D. V. Kalinin, E.V. KozharinovCIAM, Russian Federation |
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ICAS2012-P4.14: L. S. Yanovskiy, CIAM, Russian Federation FUEL CELLS ON ALTERNATIVE NON – OIL FUELS FOR GAS TURBINE ENGINES OF AN ADVANCED CIVIL AIRCRAFTS |
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ICAS2012-P4.15: V. D. Venediktov, V. G Krupa, S. V. Rudenko, et al, CIAM, Moscow, Russia THE EXPERIENCE OF HIGH PRESSURE RATIO SINGLE STAGE HPT DESIGNING |
ICAS 2012-P4.16: J. E. Barth, V. Wheatley, M. K. SmartUniv. of Queensland, Australia STREAMWISE PORTHOLE FUEL INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE |
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5. FLIGHT DYNAMICS AND CONTROL: |
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ICAS2012-P5.1: A. Tomczyk, Rzeszow Univ. of Technology, Poland MODEL FOLLOWING TOTAL IN FLIGHT SIMULATOR AS AN EDUCATIONAL TOOL |
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ICAS2012-P5.2: X. Cao, H. Li*, Luoyang Optical & Electrical Development Center, China; *Beihang Univ. (BUAA), China |
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ICAS2012-P5.3: N. Fezans, C. Kappenberger, DLR, Germany A MODEL OF HORIZONTAL TAILPLANE DAMAGE FOR USE IN FLIGHT DYNAMICS |
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ICAS2012-P5.4: C. -H. Lee, M. -J. Tahk, B. -E. Jun*, KAIST, Korea; *Agency for Defense Development, Korea AUTOPILOT DESIGN FOR AN AGILE MISSILE USING L1 ADAPTIVE BACKSTEPPING CONTROL |
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ICAS2012-P5.5: J. -W. Park, J. -H. Kim*, M. -J. Tahk, KAIST, Korea; *Rice Univ., USA UAV COLLISION AVOIDANCE VIA OPTIMAL TRAJECTORY GENERATION METHOD |
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ICAS2012-P5.6: K. Chircop, D. Zammit-Mangion*, R. Sabatini**, Univ. of Malta, Malta; *Univ. of Malta, Malta, & Cranfield Univ., UK; **Cranfield Univ., UK BI-OBJECTIVE PSEUDOSPECTRAL OPTIMAL CONTROL TECHNIQUES FOR AIRCRAFT TRAJECTORY OPTIMIZATION |
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ICAS2012-P5.7: Y. H. Hwang, M. -J. Tahk, KAIST, Korea |
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ICAS2012-P5.8: R. Takahashi, Y. Inada, Tokai Univ., Japan |
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ICAS2012-P5.9: Y. Inada, K. Ohta, H. Takanobu*, Tokai Univ., Japan; *Kogakuin Univ., Japan GUST RESPONSE ANALYSIS IN THE FLIGHT FORMATION OF UNMANNED AIR VEHICLES |
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ICAS2012-P5.10: R. Ohsawa, I. Yamamoto, N. InagawaUniv. of Kitakyushu, Japan DEVELOPMENT OF OBSERVATIONAL SYSTEM WITH UNMANNED FLIGHT SYSTEM |
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ICAS2012-P5.11: S. Celikovsky, P. Hospodar*, CTU, Prague, Czech Republic; *VZLU, Prague, Czech Republic STABILIZATION OF LONGITUDINAL AIRCRAFT MOTION USING MODEL PREDICTIVE CONTROL AND EXACT LINEARIZATION |
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ICAS2012-P5.12: O. C. Ubadike, Air Force Inst. of Technology, Nigeria FUZZY LOGIC BASED FLIGHT CONTROL SYSTEM FOR THE NIGERIAN AIR FORCE AIR BEETLE AIRCRAFT |
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6. SYSTEMS, SUBSYSTEMS AND EQUIPMENT: |
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ICAS2012-P6.1: Y. Zhu, J. Wang*, M. Jia*, Beijing Aeronautical Technology Research Centre & Beihang Univ., China; *Beijing Aeronautical Technology Research Centre, China |
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ICAS2012-P6.2: W. -C. Feng, W. -J. Song, First Aircraft Inst., China A NEW METHOD OF CALCULATION THE DELAY TIME OF MULTI-CREW MEMBER EJECTION |
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ICAS2012-P6.3: P. Paces, J. Popelka, T. Levora, Czech Technical Univ. in Prague, Czech Republic |
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ICAS2012-P6.4: J. R. Harvey, R. A. Jarvis, D. Verstraete*, et al, DSTO, Australia; *The Univ. of Sydney, Australia DEVELOPMENT OF A HYBRID-ELECTRIC POWER-SYSTEM MODEL FOR A SMALL SURVEILLANCE AIRCRAFT |
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ICAS2012-P6.5: S. -W. Shim, D. -Y. Won, M. -J. Tahk, et al, KAIST, Korea HIDDEN MARKOV MODEL PARAMETER ESTIMATION FOR MULTIPLE DIM TARGET DETECTION |
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ICAS2012-P6.6: Y. L Fu, H. T Qi, Y. L Lu*, et al, Beihang Univ. (BUAA), China; *AVIC Jincheng Nanjing Eng.Inst. Of Aircraft Systems, China A NOVEL ELECTRICAL SERVO VARIABLE DISPLACEMENT HYDRAULIC PUMP USED FOR INTEGRATED ACTUATORS IN MEA |
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ICAS2012-P6.7: G. Wild, G. Allwood, S. Hinckley, Edith Cowan Univ., Australia DISTRIBUTED OPTICAL FIBRE SMART SENSORS FOR ADVANCE SENSING SYSTEMS IN AEROSPACE VEHICLES |
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7. SYSTEMS ENGINEERING AND SUPPLY CHAIN: |
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ICAS2012-P7.1: H. Nakamura, Y. Kajikawa*, S. Suzuki, Univ. of Tokyo, Japan; *Tokyo Inst. Of Technology, Japan SCIENCE AND TECHNOLOGY MAP ANALYSIS OF AEROSPACE ENGINEERING |
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8. AIR TRANSPORT SYSTEM EFFICIENCY: |
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ICAS2012-P8.1: H. Zhou, X. Zhang, W. QinFlight Automatic Control Research Inst., Xi'an, China DEVELOPMENT OF THE OPTIMIZED APPROACH AND LANDING TRAJECTORY FOR FUTURE AIR TRANSPORT SYSTEM |
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ICAS2012-P8.2: O. J. Pinon, E. Garcia, D. N. Mavris, Georgia Inst. Of Technology, USA EVALUATING FLEXIBILITY IN AIRPORT CAPACITY-ENHANCING TECHNOLOGY INVESTMENTS |
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ICAS2012-P8.3: N. Takeichi, T. Hatano, Y. Fukuda*, Nagoya Univ., Japan; *ENRI, Japan CONTINUOUS DESCENT TRAJECTORY WITH OPTIMUM ARRIVAL TIME CONTROLLABILITY |
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ICAS2012-P8.4: P. Coughlan, Brisbane Airport Corporation, Australia |
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ICAS2012-P8.5: W. Pan, T. Chen*Civil Aviation Flight Univ. of China, China; *The Second Research Inst. of CAAC, China |
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ICAS2012-P8.6: K. Sampigethaya, R. Poovendran*, S. Taylor**, Boeing Research & Technology, USA; *Univ. of Washington, USA; **Boeing Business Jets, USA |
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ICAS2012-P8.7: S. Bagassi, D. Francia, F. Persiani, Univ. of Bologna, Italy A META-HEURISTIC APPROACH TO SIMULATE TAXI OPERATIONS |
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ICAS2012-P8.8: K. Shiomi, A. Senoguchi, S. Aoyama*, ENRI, Japan; *IRT, Japan |
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9. SAFETY AND SECURITY: |
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ICAS2012-P9.1: Y. Lemmens, L. Allain, T. Olbrechts LMS International, Belgium |
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ICAS2012-P9.2: M. Rezaei, A. Abedian, B. Teimouri*, Sharif Univ. of Technology, Iran; *Univ. of British Colombia, Canada RISK ASSESSMENT MODELLING FOR EVALUATING SAFETY AND IMPACT ON BUSINESS VIA A 3D RISK MATRIX |