CONFERENCE PROCEEDINGS

AIAC-2017-001 AN OVERVIEW ON THE USE OF COMPOSITE PARTS IN THE AEROSPACE INDUSTRY Yildirim Kemal Yillikci AIAC-2017-002 MISTAKES MADE IN LAST 8 DECADES OF STORE SEPARATION Alex Cenko AIAC-2017-003 ADAPTIVE MESH REFINEMENT AND SUB-CELL DISCONTINUITY RESOLUTION FOR HIGH ORDER DISCONTINUOUS GALERKIN DISCRETIZATIONS John Ekaterinaris AIAC-2017-004 KEY TECHNOLOGY ENABLERS TO ACHIEVE TURKISH GAS TURBINE INDUSTRY GOALS Taylan Ercan AIAC-2017-005 INTERRELATION OF MULTI-PHYSICAL PHENOMENA IN COMPOSITE MANUFACTURING PROCESSES Ismet Baran AIAC-2017-006 PERIDYNAMICS FOR PARADIGM SHIFT IN COMPUTATIONAL METHODS Erdogan Madenci AIAC-2017-007 HOW MULTIPHYSICS CAN CHANGE THE AVIATION INDUSTRY Adnan Golubovic AIAC-2017-011 DEVELOPMENT OF A TRAINING DEVICE FOR STUDENT PILOTS Tamer Savas and Tansu Filik AIAC-2017-012 NEURAL NETWORKS BASED DYNAMICAL MODEL FOR VTOL AIRCRAFT Metehan Yayla and Tugba Tuncel AIAC-2017-015 A REVIEW OF HELICOPTER REDESIGN Tugrul Oktay and Firat Sal AIAC-2017-016 RECONSTRUCTION OF WINDSIM FLOWFIELDS BASED ON PROPERORTHOGONAL DECOMPOSITION METHOD Tansu Sevine and Ismail H. Tuncer AIAC-2017-017 A MULTI AGENT PURSUIT-EVASION GAME MODEL FOR AIR ENGAGEMENT Atilla Ozpala, Mehmet Onder Efe and Hayri Sever AIAC-2017-019 FLOW CONTROL AROUND A NACA 0015 AIRFOIL WITH DBD PLASMA ACTUATOR PLACED AT CHORD DIRECTION AS VORTEX GENERATOR Rafet Gunaydin, Yahya Erkan Akansu, Hurrem Akbiyik and Mehmet Seyhan AIAC-2017-020 AN EXPERIMENTAL COMPARISON OF REAL TIME PERFORMANCES OF NONLINEAR CONTROL SCHEMES ON A 2-DOF HELICOPTER Yusuf Bugday and Mehmet Onder Efe AIAC-2017-022 UNSTEADY SOLUTION OF QUASI-1D NOZZLE USING LINEARIZED HARMONIC METHOD Arash Karshenass, Ozgur Ugras Baran and Mehmet Haluk Aksel AIAC-2017-025 AN ACTIVE ROCKET LAUNCHER CONTROLLER DESIGN FOR AN ATTACKHELICOPTER Tunc Baran Meric and Ali Turker Kutay AIAC-2017-027 AERODYNAMIC THRUST OPTIMIZATION OF A FLAPPING THIN AIRFOIL Ulgen Gulcat AIAC-2017-028 SIMULATION OF SATELLITE TWTA NONLINEARITY USING TWO QPSK CARRIERS Senol Gulgonul and Nedim Sozbir AIAC-2017-029 MECHANICAL PROPERTIES OF EPOXY BASED THERMOSET RESINS REINFORCED WITH CARBON NANOTUBE Damla Ozaslan, M.Merve Gulen, Sena Ozturk, Bahadir Turkyaman, Cihangir Duran and M.Fatih Oktem AIAC-2017-030 VIBRATION BASED FATIGUE ANALYSIS OF HELICOPTER SUPPORT STRUCTURE BY DIFFERENT METHODS Cem Genc AIAC-2017-031 AN ARTIFICIAL NEURAL NETWORK BASED ANALYSIS METHOD FOR SKIN-STRINGER STRUCTURES Anil Cankur and Ercan Gurses AIAC-2017-032 OPERATIONAL MODAL ANALYSIS IN HELICOPTER STRUCTURES CONTAINING HARMONIC EXCITATIONS Kurtulus Ersoy AIAC-2017-033 AN EXPERIMENTAL INVESTIGATION OF A PLUNGING WING UNDER GUST ENVIRONMENT Ilgin Kal, Berk Zaloglu, Idil Fenercioglu and Oksan Cetiner AIAC-2017-035 DUAL-SCHEME PROFILING TECHNIQUE FOR THE LIQUID ROCKET ENGINE NOZZLE Parviz Abdullayev and Musa Ilyasov AIAC-2017-036 CFD ANALYSIS OF HELICOPTER ROTOR IN FORWARD FLIGHT Ali Oguz Yuksel and Yusuf Ozyoruk AIAC-2017-039 OPTIMIZATION OF COMPREHENSIVE THERMAL MODEL FOR CONDUCTION COOLED ATR CHASSIS M.Sinem Sicim AIAC-2017-040 ALTERNATIVE FINITE ELEMENT BASED MODELING APPORACHES FOR CARBON NANOTUBES Oguzhan Koca, Hasan Gulasik and Ercan Gurses AIAC-2017-041 WAVE NUMBER IN TURBULENCE AND ITS DISCRETE NATURE Cahit Ciray AIAC-2017-043 TORSION TEST OF COMPOSITE BEAMS USING FIBER BRAGG GRATING SENSORS FOR STRUCTURAL HEALTH MONITORING APPLICATIONS Cansu Karatas, Boray Degerliyurt, Yavuz Yaman and Melin Sahin AIAC-2017-044 THE EFFECT OF MODAL DAMPING ON RANDOM VIBRATION METAL FATIGUE ANALYSIS Gurzap Ismail Demirel and Altan Kayran AIAC-2017-045 COMPARISON OF 2D AND 3D HOMOGENIZATION PROCESSES FOR MICROMECHANICS ANALYSIS OF UNIDIRECTIONAL COMPOSITES Mert Atasoy and Altan Kayran AIAC-2017-046 EXPERIMENTAL STUDY ON ACTIVE VIBRATION CONTROL OF A PIEZO-BEAM STRUCTURE WITH FUZZY LOGIC CONTROLLER Erdem Rahmi Senoz and Melin Sahin AIAC-2017-047 LARGE EDDY SIMULATION OF WALL-BOUNDED TURBULENT FLOWS Dogukan T. Karahan, Sarp Er and Ayse G. Gungor AIAC-2017-048 EFFECT OF WING HEATING ON FLOW STRUCTURE OF LOW SWEPT DELTA WING Gizem Sencan, Almila Guvenc Yazicioglu and Mehmet Metin Yavuz AIAC-2017-049 PANEL METHOD APPLICATIONS TO STORE SEPARATION Alex Cenko AIAC-2017-051 NONLINEAR STATIC AEROELASTIC BEHAVIOR OF COMPOSITE MISSILE FIN WITH INTERLAMINAR DAMAGE Ozge Ozkaya and Altan Kayran AIAC-2017-052 RELIABILITY ANALYSIS OF TACTICAL UNMANNED AERIAL VEHICLE (UAV) Yilmaz Koc, Baris Surucu and Nafiz Alemdaroglu AIAC-2017-053 ANALYSIS, DESIGN AND TEST OF A JET VANE BASED THRUST VECTOR CONTROL FOR TACTICAL MISSILES Oguz Eren and Sinan Eyi AIAC-2017-054 STATIC ANALYSIS OF ARBITRARILY LAMINATED COMPOSITE CANTILEVER PANELS WITH CHEBYSHEV COLLOCATION METHOD Ilke Algul , Hasan Kurtaran and Ahmet Sinan Oktem AIAC-2017-056 IN-FLIGHT MODAL IDENTIFICATION OF AN AIRCRAFT USING OPERATIONAL MODAL ANALYSIS Cagri Kocan and Evren Sakarya AIAC-2017-059 CONJUGATE HEAT TRANSFER COMPUTATIONS WITH LATTICEBOLTZMANN METHOD AND COMPARISONS ITS RESULTS WITH FINITEVOLUME METHOD Gregorio Gerardo Spinelli and Bayram Celik AIAC-2017-060 STATE-SPACE REPRESENTATION OF FLAPPING WINGS IN HOVER Ulgen Gulcat AIAC-2017-061 WIND TUNNEL TEST MATRIX DESIGN USING CFD BASED DOE Goktan Guzel, Abdullah Emre Cetiner and Ilteris Koc AIAC-2017-062 DESIGN OF A PIEZOELECTRIC ENERGY HARVESTER BY USING CYLINDER AS A BLUFF BODY Ahmet Levent Avsar and Melin Sahin AIAC-2017-064 OPTIMIZATION OF COMPLIANT PARTS OF A TRAILING EDGE CONTROL SURFACE OF A MORPHING WING Pinar Arslan and Ercan Gurses AIAC-2017-065 DUAL FRACTIONAL ORDER FEEDBACK CONTROL SYSTEM APPLIED FOR MISSILE GUIDANCE Murad Yaghi and Mehmet Onder Efe AIAC-2017-066 A REVISIT TO MUNK-MULTHOPP'S METHOD FOR ESTIMATING THE PITCHING MOMENT OF A FUSELAGE IMMERSED IN A HIGH WING FLOW Anwar Ul Haque, Waqar Asrar and Erwin Sulaeman AIAC-2017-067 EXPERIMENTAL INVESTIGATION OF FLIGHT AND PHYSICAL PARAMETERS AFFECTING THE VIBRATION RESPONSE SEVERITY OF SUBSYSTEM CARRIED BY JET AIRCRAFT Engin Metin Kaplan and Mehmet Bulent Ozer AIAC-2017-068 NUMERICAL INVESTIGATION OF INLET BOUNDARY CONDITION EFFECTS ON SECONDARY FLOWS IN LOW PRESSURE TURBINES Seyfullah Cay, and Ayse Gul Gungor AIAC-2017-070 AN OPTIMUM DEEP SUSTAINABILITY RETROFIT DESIGN ALGORITHM USING RATIONAL EXERGY MANAGEMENT MODEL: AMSTERDAM SCHIPHOL AIRPORT CASE Birol Kilkis, San Kilkis, and Siir Kilkis AIAC-2017-071 VIBRATION REDUCTION IN A HELICOPTER USING ACTIVE TWIST ROTOR BLADE METHOD INCORPORATING DIFFERENT PIEZOELECTRIC FIBER COMPOSITES Muruvvet Sinem Sicim and Levent Unlusoy AIAC-2017-072 PERFORMANCE MANAGEMENT OF DESIGN SUBCONTRACTORS BY USING ARTIFICIAL INTELLIGENCE V O Unal, A Berkol and E O Tartan AIAC-2017-074 CONSTRAINED MODEL PREDICTIVE CONTROL FOR SPACECRAFT RENDEZVOUS Ali Tevfik Buyukkocak, Suleyman Altinisik and Ozan Tekinalp AIAC-2017-075 ANALYSIS, DESIGN, AND TEST OF THE BASE ISOLATION SYSTEMS FOR SPACECRAFT TESTING SYSTEMS Mehmet Sahin AIAC-2017-076 STATIC AEROELASTIC RESPONSE PREDICTION OF TRANSPORT AIRCRAFT USING COUPLED CFD/CSD METHOD Haris Hameed Mian, Jawad Khawar, Hasan Junaid, Khurram Nisar, Wang Gang and Zhengyin Ye AIAC-2017-077 CFD BASED SOLUTIONS OF RELEASE OF GENERIC STORE Gorkem Demir and Nafiz Alemdaroglu AIAC-2017-079 CONCEPTUAL ANALYSIS AND OPTIMIZATION OF WAVERIDER BASED HYPERSONIC VEHICLE FORE-BODY INTEGRATED WITH RAMJET Najam-us-saqib and Sajid Raza Chaudry AIAC-2017-080 FLUTTER ANALYSIS OF A WING-LIKE STRUCTURE WITH PAYLOADS UTILIZING FINITE ELEMENT AND GROUND VIBRATION TEST MODES Ozgur Serin AIAC-2017-082 ONE DIMENSIONAL RADIATION HEAT FLUX CALCULATION FOR A TUBULAR COMBUSTOR Ahmet Topal, Altug Piskin and Onder Turan AIAC-2017-086 IMPLEMENTATION OF THE SUBMODELLING TECHNIQUE ON THE DOVETAIL ATTACHMENTS Ahmet Arda Akay, Demirkan Coker, Altan Kayran and Ercan Gurses AIAC-2017-087 ASSESSMENT OF PRINCIPLES FOR RPAS INTEGRATION INTONON-SEGREGATED AIRSPACE Tamer Savas and Oznur Usanmaz AIAC-2017-089 MULTIBLOCK AND PARALLEL COMPUTATIONS OF ROTOR FAN USING THREE DIMENSIONAL EULER EQUATIONS Emre Ozmen and Sinan Eyi AIAC-2017-091 KALMAN FILTER BASED LOOSELY-COUPLED GPS/INS INTEGRATION FOR BOEING-747 AIRCRAFT MODEL Chingiz Hajiyev and Deniz Burak Kamiloglu AIAC-2017-092 MEASUREMENT OF TURBULENCE LEVEL IN THE TEST SECTION OFITU TRISONIC WIND TUNNEL AT SUPERSONIC SPEEDS Hasan Tabanli, Ezgi Ede and Kemal Bulent Yuceil AIAC-2017-095 IMPLEMENTATION AND COMPARISON OF DIFFERENT POSITION SOLUTIONS OF GPS RECEIVER IN SATELLITES Ozgur Gundogan AIAC-2017-097 VORTEX CLUSTERS IN TURBULENT BOUNDARY LAYER FLOWSSUBJECTED TO ADVERSE PRESSURE GRADIENT Egemen Aydin and Ayse G. Gungor AIAC-2017-099 ENERGY AND EXERGY ANALYSIS OF UNMANNED AERIAL VEHICLE ASSIGNED SURVEILLANCE AND RECONNAISSANCE MISSION Alper Oren and C.Tahsin Yucer AIAC-2017-100 A STUDY ON ENERGY TRAPPING PARAMETERS OF A MULTISTABLE ELASTIC BEAM Ahmet Zembiloren and Ercan Gurses AIAC-2017-101 DEVELOPMENT OF AIRCRAFT IN-FLIGHT LOADS SOFTWARE WITH UNSTEADY VORTEX LATTICE METHOD (UVLM) Syed J. Ali, Haroon A. Baluch, Muhammadbilal, and Muhammad Kashif AIAC-2017-103 INVESTIGATION OF THE EFFECT OF BOUNDARY CONDITIONS ON THE BUCKLING COEFFICIENTS OF STIFFENED FLAT PANELS Enes Aydin and Altan Kayran AIAC-2017-105 DEVELOPMENT OF A BLADE TO BLADE SOLVER FOR AXIAL TURBOMACHINERY Mustafa Bilgic and Mehmet Haluk Aksel AIAC-2017-106 DEVELOPMENT OF A CYCLE DESIGN SOFTWARE FOR TURBOSHAFTENGINES Mert Erk and Mehmet Haluk Aksel AIAC-2017-107 21ST CENTURY INERTIAL NAVIGATION SYSTEMSA REVIEW OF THE LATEST TECHNOLOGIES AND TRENDS Asif Iqbal AIAC-2017-108 WING DESIGN OPTIMIZATION OF A MALE UNMANNED AERIAL VEHICLE Hudai Alayli, Halil Kaya and Senem Ayse Haser AIAC-2017-109 COMPUTATIONAL ANALYSIS OF A MODEL SCALE HELICOPTER ROTOR IN GROUND EFFECT Mehmet Sahbaz, Nilay Sezer Uzol and Dilek Funda Kurtulus AIAC-2017-110 DIA-PHONEME RELATION OF THE ATC-PILOT RADIO COMMUNICATION PHRASEOLOGY PHONETIC CONFUSION O. E. Guclu AIAC-2017-111 AIR TRAFFIC FLOW AND CAPACITY MANAGEMENT AND A NEW PROCESS FOR SLOT MESSAGE PROPOSAL Soner Demirel and Ertan Cinar AIAC-2017-112 DIFFUSION MODELS IMPLEMENTATION IN HYPERSONIC FLOW REGIMES Hilmi Berk Gur and Sinan Eyi AIAC-2017-113 INVESTIGATION OF THE PERFORMANCE OF A 2D H-DARRIEUS WIND TURBINE WITH DIFFERENT INLET GUIDE VANE CONFIGURATIONS Neset Caglar Girgin and Ozgur Erol AIAC-2017-114 SHEAR-LAYER-ADAPTED DELAYED DETACHED-EDDY SIMULATION OF A TRANSONIC OPEN CAVITY FLOW Ozgur Yalcin, Kenan Cengiz and Yusuf Ozyoruk AIAC-2017-115 EXPERIMENTAL INVESTIGATION OF A WING PERFORMING PITCH-UP MOTION UNDER GUST ENVIRONMENT Onur Son, Berk Zaloglu and Oksan Cetiner AIAC-2017-116 EVALUATION OF VERTICAL FLIGHT EFFICIENCIES DURING DEPARTURE OPERATIONS Hakki Aksoy , Oznur Usanmaz and Enis T. Turgut AIAC-2017-121 EFFECT OF WING DEFORMATION ON AERODYNAMIC LOADS AT SUPERSONIC SPEEDS Emir Ozkokdemir and Funda Kurtulus AIAC-2017-122 PERFORMANCE STUDY OF WIND TURBINES WITH BEND-TWIST COUPLED BLADES AT UNDERRATED WIND SPEEDS Oguz Atalay, Touraj Farsadi and Altan Kayran AIAC-2017-123 ALIGNMENT WORKS IN ASSEMBLY, INTEGRATION AND TESTS OF COMMUNICATION SATELLITES Mehmet Sahin, Akem Kahriman and Hakki Coskun AIAC-2017-124 FAULT DIAGNOSIS ON AIRCRAFT LONGITUDINAL FLIGHT CONTROL USING OBSERVERS Isil Yazar AIAC-2017-125 EQUIVALENT MODEL OF A SANDWICH BEAM WITH RAMP REGION UNDER FOUR POINT BENDING VIA GENETIC ALGORITHM Ozan Yardimci and Ercan Gurses AIAC-2017-126 AIRCRAFT WEAPON INTEGRATION - A STRUCTURAL VIEW Wolfgang Luber AIAC-2017-127 AIR COMBAT RULE MINING FROM MOVEMENT SEQUENCE OF FLIGHTS Mustafa Karli, Mehmet Onder Efe and Hayri Sever AIAC-2017-128 MOLECULAR DYNAMICS SIMULATIONS OF CARBON NANOTUBE REINFORCED POLYMER COMPOSITES Gozdenur Toraman, Mine Konuk, Elif Sert, Hande Ustunel, Hasan Gulasik and Ercan Gurses AIAC-2017-130 CONCEPTUAL DESIGN OF A LOW-BYPASS TURBOFAN ENGINE FOR NEXT GENERATION JET TRAINER Orcun Bulat, Olcay Sari and Onur Tuncer AIAC-2017-134 VEHICLE WIND NOISE PREDICTION THROUGH SOLUTIONS OF NAVIER-STOKES AND FFOWCS WILLIAMS AND HAWKINGS Baran Gumus, Ezgi Gunes and Yusuf Ozyoruk AIAC-2017-135 AN ARBITRARY LAGRANGIAN-EULERIAN (ALE) FRAMEWORK WITH EXACT MASS CONSERVATION FOR MULTIPHASE FLUID FLOWS Cagatay Guventurk and Mehmet Sahin AIAC-2017-138 DESIGN OF A NOVEL FOLDABLE FLAPPING WING MICRO AIR VEHICLE Can Beker, Ali Emre Turgut, Onur Ozcan, Kutluk Bilge Arikan and Dilek Funda Kurtulus AIAC-2017-139 A CARTESIAN BASED MESH GENERATOR WITH BODY FITTED BOUNDARY LAYERS Merve Ozkan, M. Haluk Aksel and Ozgur Ugras Baran AIAC-2017-140 EVALUATION OF THE SEMI-EMPIRICAL EQUATIONS OF PRESSURE SWIRL ATOMIZERS Ozan Ekin Nural and Ozgur Ertunc AIAC-2017-141 TRANSIENT FLOW SIMULATION INSIDE PRESSURE SWIRL ATOMIZER Alireza Razeghi and Ozgur Ertunc AIAC-2017-145 APPLICATION OF MILITARY AIRCRAFT STORES COMPATIBILITY IN THECIVILIAN AIRWORTHINESS REGULATORY ENVIRONMENT Malcolm Tutty, Timothy White, Graham Akroyd and Alex Cenko AIAC-2017-146 EXERGETIC BENEFITS OF CENTRAL THERMAL SYSTEM FOR SERVING PARKED AIRCRAFTS AT THE GATE San Kilkis, Siir Kilkis, and Birol Kilkis AIAC-2017-147 EXPERIMENTAL INVESTIGATIONS ON PARTICLE EROSION BEHAVIOR OF AA 6061 ALLOY Dogan Acar, Dursun Meric, Ali Ihsan Budur, Recep Gumruk, Hasan Sofuoglu, Hasan Gedikli and Omer Necati Cora AIAC-2017-148 ENERGY ABSORPTION MECHANISMS AND CRASH ANALYSIS OF HELICOPTER SEATS Gulce Ozturk and Altan Kayran AIAC-2017-149 NUMERICAL INVESTIGATION OF THE EFFECT OF THE PERMEABILITY OF EAGLES AIRFOIL ON ITS AERODYNAMICS PERFORMANCE Rania R. Rahuma, Ashraf A. Omar and Abdulhaq Emhemmed AIAC-2017-151 APPLICATION OF ANALYTIC NETWORK PROCESS IN EVALUATING INITIAL TRAINING AIRCRAFT Murat Ayar, Mustafa Cavcar and Kursad Melih Guleren AIAC-2017-152 VALIDATION OF OPEN-SOURCE CFD SOFTWARE FOR HIGH SPEED TURBULENT CAVITY FLOWS Osman Mirza Demircan, Oguzhan Demir, Seyfettin Turk and Kursad Melih Guleren AIAC-2017-153 QUANTITATIVE GRADING OF STORE SEPARATION TRAJECTORIES Kevin Jamison, Pieter Rossouw and Elizna Miles AIAC-2017-155 FLOW AROUND A SQUARE CYLINDER WITH WAVY SPLITTER PLATE PLACED UPSTREAM Mehmet Seyhan, Mustafa Sarioglu and Yahya Erkan Akansu AIAC-2017-156 A COMPUTATIONAL STUDY FOR A WING AT OR PITCHING UP TO HIGH ANGLE OF ATTACK IN PRESENCE OF A SPANWISE GUST Batuhan Eroglu, Berk Zaloglu, Oksan Cetiner and Arif Cem Gozukara AIAC-2017-157 THE EFFECT OF AIR ROUTE INTERSECTION ANGLE ON THE EFFICIENCY OF AIR TRAFFIC CONTROL OPERATIONS Ozdemir and Usanmaz AIAC-2017-159 DYNAMICAL MODELING OF A HORIZONTAL AXIS WIND TURBINE SYSTEM WITH PRECONE AND TILT ANGLES Mustafa Sahin, and Ilkay Yavrucuk AIAC-2017-162 MANAGING AIR TRANSPORT DEMAND AND CAPACITY VIA STOCHASTIC MODELLING APPROACH Baris Baspinar and Emre Koyuncu AIAC-2017-163 MULTIBODY SIMULATION OF HELICOPTER ROTOR WITH FLEXIBLE BLADE Bali Ihsan Ozturan and Altan Kayran AIAC-2017-164 DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR COMPLIANCE AND BUCKLING LOAD Hasan Inci and Altan Kayran AIAC-2017-165 COMPUTATIONAL FLUID DYNAMICS OF PERMEABLE THIN AIRFOILS Mohammed Aldheeb, Waqar Asrar, Erwinsulaeman, Ashraf A. Omar and Fadly Jashi Darsivan AIAC-2017-166 A STUDY ON CONTROLLABILITY OF AN AUGMENTED STABILITY FIGHTERAIRCRAFT Umit Kutluay, Tayfun Cimen and K. Gizem Parlak AIAC-2017-169 UNDERSTANDING HYDRODYNAMICS OF TUNA FISH HYDROFOIL USING CFD SIMULATIONS Abdullah Muratoglu and Abdurrahim Muratoglu AIAC-2017-170 HIGH GAIN OBSERVER BASED ATTITUDE CONTROL OF A QUADROTOR Metehan Yayla, Derya Kaya and Ali Turker Kutay AIAC-2017-172 AIRCRAFT ENGINE HEALTH MONITORING SYSTEM WITH NEURAL NETWORK ANALYSIS Mustagime Tulin Yildirim and Bulent Kurt AIAC-2017-173 A MULTIOBJECTIVE AERODYNAMIC OPTIMIZATION OF A MICRO SCALE VERTICAL AXIS WIND TURBINE Hakan Usanmaz and Emre Alpman AIAC-2017-179 ICING ON WIND TURBINE BLADE UNDER VARIOUS ATMOSPHERIC CONDITIONS Ozcan Yirtici, Ismail H. Tuncer and Serkan Ozgen AIAC-2017-180 ANGLE ONLY ORBIT DETERMINATION USING TELESCOPE SYSTEM Abdulkadir Koker and Ozan Tekinalp AIAC-2017-184 APPLICATION OF GENERIC AIR VEHICLE SIMULATION MODEL FOR REAL-TIME AERO-ACOUSTIC NOISE COMPUTATION OF PROPELLER AIRCRAFTS Murat Senipek, Arda Yucekayali, and Ali Turker Kutay, AIAC-2017-186 OPTIMAL GUIDANCE MODEL FOR GREEN TRAJECTYORY GENERATION OF HELICOPTERS Arda Yucekayali, Murat Senipek and Ali Turker Kutay AIAC-2017-187 ELECTROMAGNETIC AND DYNAMIC ANALYSIS OF SOLENOID ACTUATOR TO REDUCE THE CLOSING TIME Ayhan Yagci, Mehmet Polat Kuntuz, and Ozkan Bebek AIAC-2017-188 A GAME THEORETIC MODEL FOR MULTI AGENT PURSUIT-EVASION PROBLEM Atilla Ozpala, Prof. Mehmet Onder Efe, Prof and Hayri Sever AIAC-2017-195 EFFECT OF OUT-OF-AUTOCLAVE CURING ON THE BENDING STRENGTH OF TPNCF AND UNIDIRECTIONAL LAMINATES Mirac Onur Bozkurt, Kaan Bilge, Melih Papila and Demirkan Coker AIAC-2017-197 INVESTIGATION OF MEAN STRESS EFFECT FOR EQUIVALENT STRESS METHODS AND CRITICAL PLANE APPROACHES FOR HIGH CYCLE FATIGUE LIFE ESTIMATIONS Zafer Engin and Demirkan Coker AIAC-2017-198 VALIDATION AND BENCHMARKING OF COMSOL 2D AXISYMMETRIC INDUCTIVELY COUPLED ARGON PLASMA MODEL Erdal Bozkurt, Ummugul Erozbek Gungor and Nafiz Alemdaroglu AIAC-2017-199 RIME ICE SHAPE PREDICTION USING OPENFOAM Seghaer Edeeb, Hasan Akay and Serkan Ozgen AIAC-2017-201 HEAT REJECTION CAPABILITY FOR GEOSTATIONARY SATELLITES Murat Bulut and Nedim Sozbir AIAC-2017-202 NATURAL VIBRATION AND AEROELASTIC STABILITY OF REALISTIC LAUNCH VEHICLES Melahat Cihan, and Metin Orhan Kaya AIAC-2017-203 DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS Melahat Cihan, Seher Eken, and Metin Orhan Kaya AIAC-2017-204 FATIGUE LIFE ANALYSIS ON A MISSILE BODY EXPOSED TO FLIGHT LOADS Emre Okur and Kemal Yaman AIAC-2017-205 A ZERO-EQUATION TRANSITION MODEL DEPENDING ON LOCAL FLOW VARIABLES Samet Caka Cakmakcioglu, Onur Bas and Unver Kaynak