On the Dynamic Stability of a Rocket Under Constant Thrust
7. International Conference on Recent Advances in Space Technologies, 19 Haziran 2015
CİHAN MELAHAT,KAYA METİN ORHAN
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Selection Criteria for Tackifier Addition to Paraffin Wax based Hybrid Rocket Fuels
AIAA Propulsion and Energy 2019Forum, INDIANAPOLIS/AMERİKA BİRLEŞİK DEVLETLERİ, No. 3921, 19 Ağustos 2019
BİLGE KAAN, EMERCE NUR BER, YİLDİZ UTKU CAN, KOKAL UĞUR, BAYSAL MUSTAFA, KARABEYOĞLU MUSTAFA ARİF
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Effects of minimal processing and refrigerated storage on phenolic content and antioxidant capacity of rocket salad (Eruca sativa, Brassicaceae)
International Workshop on Antioxidant Measurement Assay Methods, İstanbul/TÜRKİYE, 21 Nisan 2010
TOYDEMİR ŞEN GAMZE,TACER CABA ZEYNEP,ÇAPANOĞLU GÜVEN ESRA,BOYACIOĞLU DİLEK,DEMİR NALAN
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A comparison of different antioxidant activity methods in fresh-cut rocket salad
2011 IFT Annual Meeting and Food Expo, New Orleans/AMERİKA BİRLEŞİK DEVLETLERİ, 11 Haziran 2011
TOYDEMİR ŞEN GAMZE,TACER CABA ZEYNEP,ÇAPANOĞLU GÜVEN ESRA,BOYACIOĞLU DİLEK
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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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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
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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, Aralık 2018, s. 393-399, ISSN: 0026-265X
ÖZTÜRK ELİF,MALTEPE ESRA,BAKIRDERE SEZGİN
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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
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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
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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
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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
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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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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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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
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