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Özel Aralık Girişi

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
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
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
Kadir Kırkköprü Tez Doktora Tamamlandı
Numerical simulation of unsteady flows in solid rocket motors with deforming grids
Fen Bilimleri Enstitüsü, İstanbul Teknik Üniversitesi, 2007
MURAT UYGUN
Kadir Kırkköprü Tez Doktora Tamamlandı
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
Kadir Kırkköprü 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
DIVERGENCE AND FLUTTER STABILITY BOUNDARIES OF A ROCKET MODELED AS THIN-WALLED COMPOSITE BEAMS
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, 20 Eylül 2017
CİHAN MELAHAT,EKEN SEHER,KAYA METİN ORHAN
Seher Eken Özet Bildiri
Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams
ACTA MECHANICA, Vol. 228, No. 12, 2017, s. 4353-4367, ISSN: 0001-5970
CİHAN MELAHAT,EKEN SEHER,KAYA METİN ORHAN
Development of a Design and Performance Evaluation Code of Hybrid Rocket Motors
Asian Joint Conference on Propulsion and Power, 16 Mart 2016
COSKUNPINAR ERDİ,ÖZEN KAAN,GRATE STANISLAV,ASLAN ALİM RÜSTEM
Alim Rüstem Aslan Tam metin bildiri
Robust Stabilization of Input Delayed Systems with Design Example for Rocket Motor Control
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 80, No. 1, Ocak 2008, s. 59-65, ISSN: 1748-8842
JAFAROV ELBRUS
Elbrus Jafarov Özgün Makale
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
Kadir Kırkköprü Özgün Makale
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
Kadir Kırkköprü Özgün Makale
Numerical Simulation of Flow in a Solid Rocket Motor: Combustion Coupled Pressure Dependent Regressive Boundary
International Journal of Engineering Science Invention, Vol. 6, No. 3, Mart 2017, s. 54-65, ISSN: 2319-6726
KIRKKÖPRÜ KADİR,HAVLUCU MEHMET ÖZER
Kadir Kırkköprü Özgün Makale
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
Solid rocket motor design using a surrogate model
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 7, Ekim 2018, s. 1104-1127, ISSN: 1748-8842
TOLA CEYHUN,NİKBAY MELİKE
Melike Nikbay Özgün Makale
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
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

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