- Best Paper Award Recipients:
- AIAC-2013-026
A TIME DEPENDENT FULLY COUPLED FLUID-STRUCTURE INTERACTION ALGORITHM Ali Eken and Mehmet Sahin
- AIAC-2013-154
AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINE BLADES USING A PARALLEL GENETIC ALGORITHM Ozge Polat, Nilay Sezer Uzol and Ismail H. Tuncer
- AIAC-2013-111
SURVIVABILITY ANALYSIS OF AIRCRAFT UNDER FRAGMENTATION WARHEAD THREAT Huseyin Emrah Konokman, Altan Kayran and Mustafa Kaya
- AIAC-2013-001
- PAST ACTIVITES AND RECENT EFFORTS FOR MULTIDISCIPLINARY ANALYSIS AND OPTIMIZATION IN CONCEPTUAL AND PRELIMINARY DESIGN AT CASSIDIAN
Johannes Schweiger
- AIAC-2013-003
- UNMANNED AIRCRAFT RESEARCH AT THE DLR INSTITUTE OF FLIGHT SYSTEMS - CURRENT RESEARCH AND FUTURE CHALLENGES
Joerg Dittrich
- AIAC-2013-004
- THE CONTINUOUS ADJOINT METHOD IN AERODYNAMIC SHAPE OPTIMIZATION, ROBUST DESIGN, FLOW CONTROL AND TOPOLOGY OPTIMIZATION
Kyriakos C. Giannakoglou
- AIAC-2013-005
- CONVERSION OF A CS-23 AIRPLANE TO A FLY-BY-WIRE TEST BED FOR MANNED AND UNMANNED FLIGHT CONTROL RESEARCH
Florian Holzapfel
- AIAC-2013-011
- AEROELASTIC BEHAVIOUR OF A METAL WING STRUCTURE WITH VARYING FUEL LOCATIONS.
Gamal Ashawesh, Adel Kurban and Saleh Al-khodari
- AIAC-2013-012
- DESIGN FABRICATION OF HAND LAUNCHED UAV
Adel Ali Kurban, Gamal Mohamed Ashawesh, Ahmed Assidiq Elhuni, Arij Mohammad Thabet and Hussein Farj Bizan
- AIAC-2013-013
- LONG-DISTANCE MICROPIV MEASUREMENTS OF A COMMERCIAL AIRCRAFT MODEL AT LOW REYNOLDS NUMBER
F. Gokhan Ergin and Nafiz Alemdaroglu
- AIAC-2013-014
- NUMERICAL SIMULATION OF FLUID STRUCTURE INTERACTION (FSI) EFFECT ON AN AIRCRAFT WING.
Bhuiyan Shameem Mahmood Ebna Hai
- AIAC-2013-015
- APPLICATIONS OF FAST-TRANSIENT 2ND-ORDER-ACCURATE DISCRETE-ELEMENT MODEL TO AERODYNAMIC-AEROACOUSTIC FLOWS IN SUBSONIC AND SUPERSONIC REGIMES
Arsev H. Eraslan
- AIAC-2013-016
- ANALYZING THE PDE SOLUTIONS USING OPTICAL FLOW TECHNIQUE: A CASE STUDY WITH 2D HEAT FLOW
Mehmet Onder Efe
- AIAC-2013-017
- THE EFFECT OF FILLET OF WING JUNCTION AND FRONT SHARPNESS ON THE FLOW CHARACTERISTICS OF AN X-45A TYPE UNMANNED COMBAT AIR VEHICLE
M.Murat Yavuz
- AIAC-2013-018
- FLOWFIELD DEPENDENT VARIATION (FDV) METHOD FOR FLUID-STRUCTURE INTERACTION PROBLEMS
Mohd Fadhli, Ashraf A. Omar and Waqar Asrar
- AIAC-2013-019
- API FOR DDS BASED MIL-STD-1553B BUS SIMULATOR
Sema Cam, Umut Durak, Ertan Deniz and Halit Oguztuzun
- AIAC-2013-020
- CONVERGENCE ACCELERATION OF LATTICE BOLTZMANN METHOD VIA FINITE DIFFERENCE BASED IMPLMENTATION ON UNIFORM GRIDS
Fatih Cevik, Goktan Guzel, Bedri Yagiz, Haluk Aksel and Kahraman Albayrak
- AIAC-2013-021
- PRELIMINARY DESIGN OF A TRANSONIC FAN FOR LOW BY-PASS TURBOFANENGINE
Mohamed A. Aziz, Farouk M.Owis, and Mohamed M. Abdelrahman
- AIAC-2013-022
- DESIGNING A ROBOTIC FLAPPING WING MECHANISM IN ORDER TO MIMIC THE INSECT FLIGHT
Alper Gungor, Talha Mutlu and Dilek Funda Kurtulus
- AIAC-2013-023
- EXPERIMENTAL INVESTIGATION OF FLOW THROUGH A PRESSURE SWIRL ATOMIZER AND THE RESULTING HOLLOW CONE SPRAY AT DIFFERENT OPERATING CONDITIONS
Bulent Sumer, Nejdet Erkan, Oguz Uzol and Ismail H. Tuncer
- AIAC-2013-024
- TRENDS FOR UNMANNED AERIAL VEHICLE MISSIONS AND PAYLOAD TECHNOLOGIES
Murat Tecimer, Serhat Erdemir, Erkan Gozpinar and Mert Serkan
- AIAC-2013-025
- ENGINE DESIGN MODEL FOR SEPERATE FLOW TURBOFAN ENGINES
I.Sinan Akmandor and S.Can Uysal
- AIAC-2013-026
- A TIME DEPENDENT FULLY COUPLED FLUID-STRUCTURE INTERACTION ALGORITHM
Ali Eken and Mehmet Sahin
- AIAC-2013-027
- A QUAD-TREE BASED AUTOMATIC ADAPTIVE CARTESIAN GRID GENERATOR WITH APPLICATIONS ON MULTI-ELEMENT AIRFOILS
Emre Kara, Ahmet Ihsan Kutlar and Mehmet Haluk Aksel
- AIAC-2013-028
- MACH SWEEP TECHNIQUE FOR STORE SEPARATION WIND TUNNEL TESTING
Alex Cenko, Murray Snyder and Graham Doig
- AIAC-2013-029
- DESIGN OPTIMIZATION OF A TRANSONIC-FAN ROTOR USING NUMERICALCOMPUTATIONS OF THE FULL COMPRESSIBLE NAVIER-STOKES EQUATIONS AND SIMPLEX ALGORITHM
Mohamed A. Aziz, Farouk M. Owis and Mohamed M. Abdelrahman
- AIAC-2013-031
- FAVRE AVERAGED NAVIER-STOKES EQUATIONS AGAIN
Cahit Ciray
- AIAC-2013-032
- ENGINE DESIGN FOR A HALF SCALE MODEL OF JSF UAV WITH HIGH POWER EXTRACTION REQUIREMENTS
Cihat Akin, Cosku Catori, Oguz Eren, Burak Ozkahya and Onur Tuncer
- AIAC-2013-033
- TECHNOLOGY ROADMAPS - AN AEROSPACE APPLICATION
Gozde Kara, Eyup Serdar Gokpinar and Erhan Solakoglu
- AIAC-2013-035
- FLIGHT SIMULATION OF A HIGH WING UNMANNED AERIAL VEHICLE
Amir Teimourian and Dariush Firouzbakht
- AIAC-2013-036
- DIRECT NUMERICAL SIMULATION OF COMBINED EFFECTS OF WAKE AND DISCRETE SURFACE ROUGHNESS ON SEPARATED BOUNDARY LAYERS
Suleyman Karaca, Mark P. Simens and Ayse G. Gungor
- AIAC-2013-038
- ENERGY HARVESTING STUDIES ON FIN LIKE STRUCTURE VIA PIEZOELECTRIC MATERIAL
Ahmet Levent Avsar and Melin Sahin
- AIAC-2013-039
- GEOMETRIC NONLINEAR AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO WINGS
Omar S.Habib, Mohammad N.Abuelfoutouh and Hani M.Negm
- AIAC-2013-040
- DEVELOPMENT OF A NAVIER-STOKES SOLVER FOR HIGH-FIDELITY SIMULATION OF WIND TURBINE NOISE
Kenan Cengiz and Yusuf Ozyoruk
- AIAC-2013-042
- DESIGN OF A DEPLOYABLE UAV
Joshua Jackson, Rafic Ajaj, and Michael Friswell
- AIAC-2013-043
- AN INTERNAL COOLING TEST BENCH FOR GAS TURBINE RESEARCH
Sinan Inanli, Tolga Yasa, Yavuzer Karakus and Isa Kavas
- AIAC-2013-045
- CREEP LIFE IMPROVEMENT BY REDESIGNING OF A TURBINE STAGE
Cihat Akin and Tolga Yasa
- AIAC-2013-046
- SPACECRAFT ATTITUDE DETERMINATION BASED ON GPS CARRIER PHASE MEASUREMENTS
Evrim Ozten and Ozan Tekinalp
- AIAC-2013-047
- RELIABILITY BASED DESIGN OPTIMIZATION OF SOLAR ARRAYS OF A LOW EARTH ORBIT NANO-SATELLITE MISSION
Egemen Mentes, Mertcan Bayar, Dogacan Su Ozturk, Pinar Acar and Melike Nikbay
- AIAC-2013-048
- SIMULATED FLUTTER TEST OF WINGS
Taner Birtan Balevi and Altan Kayran
- AIAC-2013-049
- A 2-D THEORETICAL AND COMPUTATIONAL STUDY FOR PRELIMINARYDETERMINATION OF GRID FIN GEOMETRIC PARAMETERS AT LOW TRANSONIC SPEEDS
Erdem Dikbas, Ozgur Ugras Baran and Cuneyt Sert
- AIAC-2013-050
- DAMAGE TOLERANCE EVALUATION OF AN AIRCRAFT FUSELAGE PANEL CONTAINING A BROKEN STRINGER
M. Burak Sayar and Altan Kayran
- AIAC-2013-051
- ADAPTIVE SLIDING MODE CONTROLLER DESIGN OF A TURBOSHAFT ENGINE
Erkan Abdulhamitbilal
- AIAC-2013-052
- MODELING THE FLIGHT DYNAMICS OF A NEW SUPERSONIC AIRCRAFT DURING PRELIMINARY DESIGN
Kasim Biber
- AIAC-2013-053
- EFFECT OF BLADE-TIP GEOMETRY ON TURBINE LOSSES AND FILM OOLING EFFECTIVENES
Ahmed M. Elsayed, Farouk M. Owis and Mohamed M. Abdelrahman
- AIAC-2013-054
- MORPHING AIRCRAFT: THE NEED FOR A NEW DESIGN PHILOSOPHY
Rafic Ajaj, Andy Keane, Chris Beaverstock, Michael Friswell and Daniel Inman
- AIAC-2013-055
- LINEARIZED STRUCTURAL DYNAMICS MODEL FOR THE SENSITIVITY ANALYSIS OF HELICOPTER ROTOR BLADES
Aykut Tamer and Pierangelo Masarati
- AIAC-2013-056
- MODELING AND SIMULATION OF COAXIAL-ROTOR HELICOPTERAERODYNAMICS IN HOVER AND FORWARD FLIGHT
Murat Gecgel and Oktay Baysal
- AIAC-2013-057
- EXPERIMENTAL AEROELASTIC ANALYSIS OF A TAPERED WING WITH EXTERNAL STORE CONSIDERING THE EFFECTIVE PARAMETERS
H.Golparvar, M.Mousavi, S.Irani and B.Hassani
- AIAC-2013-058
- EFFECTS OF DURATION OF LASER ENERGY DEPOSITION ON SUPERSONICCAVITIES AND SENSOR PLACEMENT STRATEGIES FOR FLOW CONTROL
Ibrahim Yilmaz and Selin Aradag
- AIAC-2013-059
- DEVELOPMENT AND ANALYSIS OF FLAT PLATE IN FLAPPING MOTION USING PIEZOELECTRIC ACTUATORS
Ozgur Harputlu and D.Funda Kurtulus
- AIAC-2013-061
- DESIGN OF AUTONOMOUS UNMANNED AERIAL ROBOTIC VEHICLE FOR THE INTERNATIONAL FUTURE FLIGHT DESIGN COMPETITON-2013
Dilek Basaran Bil
- AIAC-2013-064
- DYNAMIC RESPONSE OF THE FGM PLATES TO BLAST LOADING
Vedat Z. Dogan
- AIAC-2013-065
- TIME DOMAIN SYSTEM IDENTIFICATION FOR AN UAV USING FLIGHT TEST DATA
Senem Ayse Haser
- AIAC-2013-066
- A MULTIPLE-LOOP AIRCRAFT FLIGHT CONTROLLER USING SDRE TECHNIQUE
Ozan Tekinalp and Anna Prach
- AIAC-2013-067
- DEVELOPMENT OF TWO NONLINEAR CONTROLLERS FOR THE CONTROL OF AIRCRAFT FORMATIONS
Segun Ariyibi and Ozan Tekinalp
- AIAC-2013-068
- EXTERNAL GEOMETRY AND FLIGHT PERFORMANCE OPTIMIZATION OF A TURBOJET PROPELLED AIR TO GROUND MISSILE
Emre Dede and Ozan Tekinalp
- AIAC-2013-069
- OPTIMIZATON OF A MORPHING WING FOR RANGE
Durmus Sinan Korpe and Serkan Ozgen
- AIAC-2013-070
- FLUCTUATING PRESSURE MEASUREMENTS IN A INLET-ISOLATOR MODEL IN MACH 2 FLOW
Hasan Tabanli and Kemal Bulent Yuceil
- AIAC-2013-071
- INVESTIGATION OF HYDRODYNAMIC CHARACTERISTICS OF AN AUV BY USING A NEW DEVELOPED CFD ANALYSIS MODEL
Sertac Arslan, Hayri Acar and Mehmet Serif Kavsaoglu
- AIAC-2013-072
- NEW APPROACH TO NAVIGATION :FROM CONVENTIONAL SYSTEMS TO SATELLITE SYSTEMS
Alper Oren and Zeynep Seda Mor
- AIAC-2013-074
- CONTINUOUS FIBER PATH OPTIMIZATION IN COMPOSITE STRUCTURES
Hasan Inci and Altan Kayran
- AIAC-2013-075
- DEVELOPMENT OF AN EXTERNAL BALLISTIC SIMULATION SOFTWARE
Serkan Berkay Korpe and Mehmet Haluk Aksel
- AIAC-2013-076
- STRUCTURAL AIRCRAFT DESIGN: WAKE PENETRATION EFFECTS ON DYNAMIC LOADS
Wolfgang Luber
- AIAC-2013-077
- AEROELASTIC INSTABILITY OF AIRCRAFT WINGS MODELED AS THIN-WALLED COMPOSITE BEAMS
Seher Durmaz and Metin O. Kaya
- AIAC-2013-079
- DESIGNING AND TESTING OF A 1.5 KW HALL EFFECT THRUSTER
Erdal Bozkurt and Nafiz Alemdaroglu.
- AIAC-2013-081
- AIRCRAFT POSITION AND VELOCITY DETERMINATION BASED ON GPS MEASUREMENTS USING DISTANCE DIFFERENCE AND DOPPLER METHODS
Oguz Eren and Chingiz Hajiyev
- AIAC-2013-082
- DYNAMIC FINITE ELEMENT ANALYSIS OF AN AIRCRAFT SEAT
Gokay Simitcioglu and Vedat Z. Dogan
- AIAC-2013-083
- MAINTENANCE OF AN AIRCRAFT DURING PROTOTYPING PHASE
Necmi Kara and Mahmut Mazmanci
- AIAC-2013-084
- TWO LEVEL OPTIMIZATION OF FIBER-PLACED LAMINATED CYLINDRICAL SHELLS OF REVOLUTION
Sedat Guldu, Altan Kayran, Gokhan Tursun and Anil Kockar
- AIAC-2013-085
- AN EXPERIMENTAL STUDY ON ACTIVE FLOW CONTROL OVER S809 AIRFOIL USING SYNTHETIC JET ACTUATORS
Melika Gul, Oguz Uzol and I. Sinan Akmandor
- AIAC-2013-086
- FUTURE FLIGHT DESIGN (FFD): AN INTERNATIONAL COMPETITION ON DESIGNING AERIAL ROBOTIC VEHICLES FOR THE FUTURE
Y. Volkan Pehlivanoglu and Abdurrahman Hacioglu
- AIAC-2013-087
- THE SIMULATION OF ATTITUDE CONTROLLER DESIGN FOR A QUADROTOR MODEL VIA SEVERAL METHODS FROM LITERATURE
Emre Yilmaz and Ali Turker Kutay
- AIAC-2013-088
- RELIABILITY ESTIMATION OF A HORIZONTAL AXIS WIND TURBINE USING TAIL MODELING
Nehir Kandemir and Erdem Acar
- AIAC-2013-089
- MODELING, SIMULATION AND SYSTEM IDENTIFICATION OF A QUADROTOR HELICOPTER
Derya Kaya and Ali Turker Kutay
- AIAC-2013-090
- THERMAL ANALYSIS FOR NOZZLE GUIDE VANE OF A SMALL SCALE GAS TURBINE ENGINE
Nadir Kacar, Volkan Tatar, Haydar Aras and L.Berrin Erbay
- AIAC-2013-091
- FFD 2013 MODEUS AIRCRAFT
Seyhan Gul, Mehmet Sahbaz, Sudeyf Musayev, Umut Gurkan, Olcay Alptug Akdag, Arda Yuksel, Semih Soganci, Deniz Karataban, Misra Ayse Adsiz, Serap Adakul, Levent Cevher, Volkan Cosgun, Dilek Funda Kurtulus and Ozan Tekinalp
- AIAC-2013-092
- EFFECTS OF WINGLET ON THE AEROELASTIC CHARACTERISTICS OF A UAV
Evren Sakarya and Umut Susuz
- AIAC-2013-094
- WIND POTENTIAL ESTIMATIONS BASED ON UNSTEADY TURBULENT FLOW SOLUTIONS COUPLED WITH A MESOSCALE WEATHER PREDICTION MODEL
Engin Leblebici, Gokhan Ahmet and Ismail H. Tuncer
- AIAC-2013-095
- COMPUTATIONAL MODELING OF VISCOELASTIC TWO-PHASE SYSTEMS
Daulet Izbassarov, Metin Muradoglu and Hadi Nozari
- AIAC-2013-097
- DESIGN AND MANUFACTURING OF THE SINGLE LANGMUIR PROBE FOR PLASMA MEASUREMENTS IN HALL EFFECT THRUSTER EXPERIMENTS
Ozge Tabak and Nafiz Alemdaroglu
- AIAC-2013-098
- DESIGN AND OPTIMISATION OF HIGH SPEED PROJECTILE NOSE GEOMETRY FOR MAXIMUM EFFECTIVENESS AND STABILITY
Osman Basoglu and Ozgur Ugras Baran
- AIAC-2013-099
- PASSIVE FLOW CONTROL IN SEMI-SUBMERGED ENGINE INLETS AT TRANSONIC FLOWS.
Ozgur Ugras Baran
- AIAC-2013-100
- FIN MIXING OPTIMIZATION TO MINIMIZE CONTROL COUPLING EFFECTS
Umit Kutluay
- AIAC-2013-103
- AN INTEGRATED STORE SEPARATION ANALYSIS TOOL
Kenan Unal and Ozgur Ugras Baran
- AIAC-2013-104
- AERODYNAMIC PERFORMANCE EVALUATION OF A WIND TURBINE ROTOR
Yuksel Ortakaya, Alper Ezertas, Ozge Polat and Taylan Cakiroglu
- AIAC-2013-105
- DESIGN PROCESS OF AN UAV FOR AIAA DBF 2013 COMPETITION
Murat Senipek, Metehan Yayla, Afif Umur Limon, Ramin Rouzbar, Yosheph Yosheph, Ugur Kalkan, Niyazi Senol, Ezgi Akel, Osman Gungor, Batuhan Hos, Ayse Usta, Ismail Ozdemir Uzunlar, Selahattin Burak Sarsilmaz and Dilek Funda Kurtulus
- AIAC-2013-106
- LNG AS AN ALTERNATIVE AVIATION FUEL: INCORPORATING MEMBRANE TYPE CRYOGENIC WING TANKS WITH A CENTRAL CRYOGENIC PRESSURE VESSEL FOR AIRBORNE LNG STORAGE AND FUELLING
Caglar Ucler
- AIAC-2013-107
- FLUTTER CHARACTERISTICS OF AN ADAPTIVE WING HAVING CAMBER CHANGE AND FREEPLAY NONLINEARITY
Levent Unlusoy and Yavuz Yaman
- AIAC-2013-108
- DYNAMIC STABILITY FLIGHT TESTS OF REMOTE SENSING MEASUREMENT CAPABLE AMPHIBIOUS UNMANNED AERIAL VEHICLE (A-UAV)
Metehan Yayla, Selahattin Burak Sarsilmaz, Talha Mutlu, Volkan Cosgun, Bedri Kurtulus, D. Funda Kurtulus and Ozan Tekinalp
- AIAC-2013-109
- LARGE EDDY SIMULATION OF COMPRESSIBILE FLOW AROUND NACA 0012 AIRFOIL AT STALL CONDITION
Farshad Rezaei, Ehsan Roohi and Mahmoud Pasandideh-fard
- AIAC-2013-111
- SURVIVABILITY ANALYSIS OF AIRCRAFT UNDER FRAGMENTATION WARHEAD THREAT
Huseyin Emrah Konokman, Altan Kayran and Mustafa Kaya
- AIAC-2013-112
- THE EFFECT OF FIBER ORIENTATION ANGLE AND PLY THICKNESS ON SUBSONIC AND SUPERSONIC FLUTTER CHARACTERISTICS OF A COMPOSITE MISSILE FIN
Ceyhun Tola and Altan Kayran
- AIAC-2013-113
- OPTIMISING MISSION PERFORMANCE FOR A MORPHING MAV
Christopher S. Beaverstock, Rafic M. Ajaj, Michael I. Friswell, Roeland De Breuker and Noud P. M. Werter
- AIAC-2013-114
- VIBRATION ANALYSIS OF A ROTATING THIN-WALLED COMPOSITE BLADE
Seher Durmaz, Ozge Ozdemir and Metin O. Kaya
- AIAC-2013-116
- NONLINEAR PERFORMANCE EVALUATION OF ALTITUDE AUTOPILOT DESIGNED VIA ROOT LOCUS COMPENSATION
Ahmet Sofyali and Elbrous M. Jafarov
- AIAC-2013-119
- DETERMINATION OF PRYING LOAD ON BOLTED CONNECTIONS
Mert Atasoy and Altan Kayran
- AIAC-2013-120
- FREQUENCY DOMAIN SYSTEM IDENTIFICATION OF AN UAV FROM FLIGHT TEST DATA
Orkun Simsek and Ozan Tekinalp
- AIAC-2013-121
- THE GROUND EFFECT ON THIN AIRFOILS AND WINGS
Ulgen Gulcat
- AIAC-2013-124
- AEROELASTIC AND CONTROL SYSTEM MODELING OF A MISSILE CONTROL FIN FOR AEROSERVOELASTIC ANALYSIS
Mehmet Ozan Nalci and Altan Kayran
- AIAC-2013-125
- DEVELOPMENT OF AN AEROSERVOELASTIC MATHEMATICAL MODEL OF A MISSILE CONTROL FIN
Mehmet Ozan Nalci and Altan Kayran
- AIAC-2013-129
- COMPUTATIONAL EVALUATION OF C-130 DRAG REDUCTION WITH AFT BODY MODIFICATIONS
Erdem Ayan, Hakan Telli and Y. Volkan Pehlivanoglu
- AIAC-2013-132
- A DESIGN TOOL FOR THE PRELIMINARY ANALYSIS OF GAS TURBINE COMBUSTORS
Ahmet Topal, Sitki Uslu and Onder Turan
- AIAC-2013-134
- UNMANNED AIR VEHICLE OF ERCIYES UNIVERSITY
Murat Onay, I. Kurtulus Ciklaiblikci and Muzaffer Ozkoca
- AIAC-2013-135
- DSP-BASED FLIGHT CONTROLLER DESIGN FOR AN UNMANNED AERIAL VEHICLE
Berk Korkut and Ozan Tekinalp
- AIAC-2013-136
- AN EXTENSIVE STRUCTURAL MAINTENANCE PROBLEM CAUSED BY CORROSION ON AN AIRCRAFT
Mustafa Sahin, Murat Ekici and Huseyin Demirci
- AIAC-2013-139
- THRUST GENERATION OF PLUNGING AIRFOILS IN TANDEM AND BIPLANE CONFIGURATIONS
S. Banu Yucel, Mehmet Sahin and M. Fevzi Unal
- AIAC-2013-140
- MISSILE AERODYNAMIC PARAMETER ESTIMATION
Arda Aksu
- AIAC-2013-141
- DESIGN AND PERFORMANCE OF WING CONFIGURATIONS FOR HIGH ALTITUDE SOLAR POWERED UNMANNED SYSTEM
Erdinc Mermer, Abdulkadir Koker, Erdal Yilmaz and D. Funda Kurtulus
- AIAC-2013-142
- WHIRL TOWER TESTING AND HOVER PERFORMANCE EVALUATION OF A 3 METER RADIUS ROTOR DESIGN
Arda Yucekayali, Alper Ezertas and Yuksel Ortakaya
- AIAC-2013-143
- FINITE-DIFFERENCE IMPLEMENTATION OF LATTICE BOLTZMANN METHOD FOR USE WITH NON-UNIFORM GRIDS
Fatih Cevik, Goktan Guzel, Bedri Yagiz, Haluk Aksel and Kahraman Albayrak
- AIAC-2013-147
- COMPUTATIONAL SIMULATIONS OF SHOCK WAVE LAMINAR BOUNDARY LAYER INTERACTION
Hasan Avsar, Ali At and Bayram Celik
- AIAC-2013-148
- VIBRATIONS OF STRUCTURES CONTAINING CRACKS
Dilek Basaran Bil
- AIAC-2013-150
- DESIGN PROCESS OF AN AUTONOMOUS MODULAR UAV (HUKUMDAR)
Halil Ibrahim Gucluberat Olcerali Goksunrecep Salimburhanettin Koyuncuertugrul Cihat Sunguryusuf Payalankazim Almacifurkan Ozturkali Riza Ekenzafer Kazanciabdurrahman Hacioglu
- AIAC-2013-151
- STRUCTURAL ANALYTICAL CONTROL PROGRAM FOR C-130 FLEET OF TURKISH AIR FORCE
Yavuz Nacakli and Zekeriya Karadurmus
- AIAC-2013-152
- TAI ROTARY WING UAV (R-300) DEVELOPMENT AND TESTING ACTIVITIES
Sahika Ozdemİr, Mahmut Bİlgİn, Selim Kocabay and Bulent Korkem
- AIAC-2013-154
- AERODYNAMIC SHAPE OPTIMIZATION OF WIND TURBINE BLADES USING A PARALLEL GENETIC ALGORITHM
Ozge Polat, Nilay Sezer Uzol and Ismail H. Tuncer
- AIAC-2013-155
- ATTITUDE ESTIMATION OF A RIGID BODY FROM INERTIAL/MAGNETIC MEASUREMENTS USING EXPONENTIAL COORDINATES
Vahid Bashiribargoshadi and Ali Turker Kutay
- AIAC-2013-156
- TAI ROTARY WING UAV MODELING AND FLIGHT CONTROL SYSTEM DEVELOPMENT
Volkan Kargin, Baris Yalcin, Umut Ture, Deniz Karakas and Ethem Hakan Orhan
- AIAC-2013-157
- STRUCTURAL MODIFICATION AND SYSTEM INTEGRATION OF CONVERTING SINGLE SEAT MANNED HELICOPTER TO AN AUTOMATED UNMANNED HELICOPTER
Bilgin Celik and Hasan Sarac
- AIAC-2013-158
- CARBON FIBER REINFORCED POLYMER BASED UAV SYSTEM DESIGNED FOR FFD 2013
Gizem Sencan, Murat Bozdemir, Fatime Zehra Kose and Huseyin Lekesiz
- AIAC-2013-160
- COMPARISON OF AERODYNAMIC DESIGN METHODOLOGIES FOR MORPHING UAV WINGS
Andrea Ciarella, Marco Hahn, Peter Wong and Andrew Peace
- AIAC-2013-161
- A NOVEL NONRECLECTING BOUNDARY CONDITION FOR ONE DIMENSIONAL UNSTEADY FLOW
Baha Zafer and Can Fuat Delale
- AIAC-2013-162
- PARALLEL IMPLEMENTATION OF DETACHED EDDY SIMULATION ON 2D HYBRID GRIDS
Ozcan Yirtici and Ismail H. Tuncer
- AIAC-2013-163
- NUMERICAL AND EXPERIMENTAL INVESTIGATION OF A PRESSURE SWIRL ATOMIZER FLOW FIELD
Bora Yazici, Oguz Uzol
- AIAC-2013-164
- 2013 DBF KASIF 3 AIRCRAFT DESIGN AND LEARNING OUTCOMES
Ahmet Ermeydan and Gokhan Durmus
|