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Toplam 23 adet sonuçtan 20 tanesi görüntülenmektedir.

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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
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
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
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
İbrahim Özkol Özgün Makale
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
Nazım Kemal Üre Tam metin bildiri
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
Alim Rüstem Aslan Tez Yüksek Lisans Tamamlandı
Development of novel hybrid rocket internal ballistic configuration for in-space applications
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2022
MEHMET KAHRAMAN
İbrahim Özkol Tez Doktora Tamamlandı
A mathematical model for prediction of film cooling performance in liquid propellant rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
AKIN SÖZERİ
Seyhan Onbaşıoğlu Tez Yüksek Lisans Tamamlandı
Pressure regulator design for liquid propellant rocket engines
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2023
ÇAĞRI İNANÇ
Alim Rüstem Aslan Tez Yüksek Lisans Tamamlandı
HIGH TEMPERATURE DRIVEN OPTIMIZATION OF A HYBRID ROCKET GRAPHITE NOZZLE DESIGN
Lisansüstü Eğitim Enstitüsü, İstanbul Teknik Üniversitesi, 2024
ŞULE ÖZTÜRK
İbrahim Özkol Tez Yüksek Lisans Tamamlandı
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
Alim Rüstem Aslan Tez Yüksek Lisans Tamamlandı
Supersonic jet-wall interactions in model rocket launchers
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 1998
METİN UÇAK
İlyas Bedii Özdemir Tez Yüksek Lisans Tamamlandı
The effects of the shape of the fore body on the flow behind the rocket body
Seventh Triennial International Symposium on Fluid Control (FLUCOME’03), Measurement and Visualization, 25 Ağustos 2003
DOLEK OMER,ÖZDEMİR İLYAS BEDİİ
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
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
Seher Eken Tam metin bildiri
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
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
Metin Orhan Kaya Tam metin bildiri
Prediction of Cool-Down Time of a Solid Rocket Motor by a Surrogate Model
AIAA Aviation and Aeronautics Forum and Exposition, Denver/AMERİKA BİRLEŞİK DEVLETLERİ, 5 Haziran 2017
TOLA CEYHUN,NİKBAY MELİKE
Melike Nikbay Tam metin bildiri
Investigation of the Effects of Slotted Solid Propellant s Sectional Geometry on Structural Strength and Internal Ballistic Performance of a Rocket Motor
6th EASN International Conference on Innovation in European Aeronautics Research, porto/PORTEKİZ, 18 Ekim 2016
TOLA CEYHUN,NİKBAY MELİKE
Melike Nikbay Tam metin bildiri roketkati yakit
Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method
7th International Conferenceon Recent Advances in Space Technologies, Istanbul/TÜRKİYE, 16 Haziran 2015
CEYHUN TOLA,NİKBAY MELİKE
Melike Nikbay Tam metin bildiri FlutterRoket

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