DYNAMIC AND STRUCTURAL ANALYSIS OF ROCKET LAUNCH SYSTEMS
INTERNATIONAL GRADUATE RESEARCH SYMPOSIUM, İSTANBUL/TÜRKİYE, 1 Haziran 2022
ERGÜN FEYZA, OZKOL İBRAHİM, SEZENOĞLU FULİN, DEMİR ESRA
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Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis
Journal of Spacecraft and Rockets, Vol. 56, No. 2, Mart 2019, s. 498-516, ISSN: 0022-4650
TOLA CEYHUN,NİKBAY MELİKE
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Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach
Journal of Spacecraft and Rockets, Vol. 55, No. 4, Temmuz 2018, s. 936-947, ISSN: 0022-4650
TOLA CEYHUN,NİKBAY MELİKE
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Hybrid Rocket Nozzle Erosion with Microaluminum-Added Fuel
Journal of Propulsion and Power, Vol. 38, Kasım 2022, ISSN: 2022-08-23
KARAKAŞ HAKKI, KAHRAMAN BÜŞRA, OZKOL İBRAHİM, KARABEYOĞLU MUSTAFA ARİF
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Modeling and Simulation of Aerobee 150A Sounding Rocket
AIAA Modeling and Simulation Technologies Conference, 9 Ocak 2017
AKÇAL MEHMET UĞUR,YUKSEK BURAK,ÜRE NAZIM KEMAL
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Design and optimization of two stage launch vehicles with the same liquid propellant rocket engines in both stages
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2022
KUBİLAY ÖZÇELİK
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A mathematical model for prediction of film cooling performance in liquid propellant rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
AKIN SÖZERİ
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PRESSURE REGULATOR DESIGN FOR LIQUID PROPELLANT ROCKET ENGINES
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
ÇAĞRI İNANÇ
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Development of novel hybrid rocket internal ballistic configuration for in-space applications
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2022
MEHMET KAHRAMAN
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Preliminary design tool for hybrid rocket engine powered leo nanosat launch vehicle and its application
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2019
NAZMİ ERDİ COŞKUNPINAR
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Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
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Investigation of compressible flow inside solid propellant rocket motor combustion chamber using various turbulence closure models
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2005
ULAŞ GÜNEŞ YÜKSEL
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Numerical simulation of unsteady flows in solid rocket motors with deforming grids
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
MURAT UYGUN
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A numerical study on the interaction of flow and combustion in solid propellant rocket motors
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2017
MEHMET ÖZER HAVLUCU
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Numerical Simulation of Flow in a Solid Rocket Motor Combustion Coupled with Regressive Boundary
Journal of Multidisciplinary Engineering Science and Technology, Vol. 3, No. 1, Ocak 2016, s. 3790-3798, ISSN: 3159-0040
HAVLUCU MEHMET ÖZER,KIRKKÖPRÜ KADİR
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Unsteady vorticity generation and evolution in a model of a solid rocket motor
Journal of Propulsion and Power, Vol. 12, No. 4, Temmuz 1996, s. 646-654, ISSN: 0748-4658
KIRKKÖPRÜ KADİR,KASSOY DAVİD R,QİNG ZHAO
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DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 20 Eylül 2017
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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A novel analytical method for the determination of cadmium in sorrel and rocket plants at ultratrace levels: Magnetic chitosan hydrogels based solid phase microextraction-slotted quartz tube-flame atomic absorption spectrophotometry
MICROCHEMICAL JOURNAL, Vol. 143, No. null, 2018, s. 393-399, ISSN: 0026-265X
ÖZTÜRK ELİF,MALTEPE ESRA,BAKIRDERE SEZGİN
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Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, Aralık 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara/TÜRKİYE, 20 Eylül 2017
CİHAN MELAHAT, EKEN SEHER, KAYA METİN ORHAN
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