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Article Transformation Induced Plasticity (trip) of Sae 52100 Steel During Martensitic and Bainitic Transformations(2017) Şimşir, CanerTransformation induced plasticity (TRIP) of SAE 52100 steel during quenching is investigatedboth experimentally and theoretically. TRIP parameter (K) is determinedexperimentally for both martensitic and bainitic transformations by using the stresseddilatometry technique. A new method for extraction of for an incomplete transformationis suggested for the martensitic transformation. Theoretical calculations using wellestablishedmodels for the TRIP effect and the results from the literature are used forthe justification of the results of this work. The results for bainitic transformation isfound to be in good agreement with both the literature and theoretical calculations usingLeblond`s model. On the other hand, experimentally determined value is found to besignificantly different from the literature. Nevertheless, it is still in reasonable agreementwith the calculations using Leblond`s model.Article İKİ KATMANLI DOLU BİR SİLİNDİRİN ELASTİK DAVRANIŞININ FARKLI UÇ VE SINIR KOŞULLARI İÇİN ANALİTİK OLARAK İNCELENMESİ(Turkish Soc thermal Sciences Technology, 2020) Akış, Tolga; Eraslan, Ahmet N.İki katmanlı dolu silindirlerin zamana bağlı termoelastik davranışlarının farklı uç ve sınır koşulları için belirlenmesi amacıyla analitik modeller geliştirilmiştir. Söz konusu silindirler, aralarında mükemmel temas olan ikikatmandan oluşmaktadır. Başlangıçta sıcak olan silindir, yüzeyinden konveksiyon yolu ile sıfır derecelik çevreselsıcaklığa veya önceden daha düşük olarak belirlenen yüzey sıcaklığına ulaşana kadar enerji kaybetmektedir. Tümdurumlarda soğuma yavaş bir biçimde gerçekleştiğinden problemde kuplajsız elastisite teorisinin kullanılması mümkünolmuştur. Genelleştirilmiş düzlemsel şekil değiştirme çözümü elde edilmiş ve bu çözüm, eksenel yöndeki birim şekildeğiştirmeyi sıfıra eşitleyerek düzlemsel şekil değiştirme durumuna ait çözüme indirgenmiştir. Bu çözümlere aitsonuçlar, sınır koşullarının serbest olduğu durumlarda radyal ve teğetsel yöndeki gerilmelerin uç koşullarına göredeğişmediğini göstermiştir. Ancak düzlemsel şekil değiştirme durumunda, eksenel gerilme baskın gerilme olmakta veuçların serbest olduğu duruma göre oldukça yüksek değerlere ulaşmaktadır. Kompozit silindirin eksenel ve radyalyönde yer değiştirmesinin kısıtlanması büyük gerilmelere yol açmasına rağmen ilgili gerilme durumu silindirde akmayayol açmamaktadır.Article Launching To an Orbit With a Chemical Propellant Staged Rocket Systems(2022) Inger, Erk; Inger, ErkThere is one way to explore space by using the space launch vehicles, which is known as rockets, and it can carry useful load named simply as payload of satelite from Earth into Space. In this study, performance predictions of the multi rocket motors are discussed and compared with single rocket motor with the same amount of propellant used for space travel. In this article in serial or tandem staging schemes, the boosting stage is usually the largest, the second stage and subsequent upper stages are above it, usually decreasing in size are used. In boosting stage parallel staging schemes solid or liquid rocket boosters are used to assist with launch. At low level starting to high altitude higher density fuel solid fuels, kerogen and cryogenic hydrogen(-250°C) are used as fuel. In solid propellants oxidizer is generally ammonium per chloride is used but in cryogenic liquid propellants oxygen(183.3°C) are used. In the first stage, both liquid propellant in a booster and five solid rocket propellent are used to reach about a certain altitude and velocity. In second stage, after reducing the weight by ejecting the five solid rocket propellent and only liquid propellant is used only to reach the an extra altitudes and velocities at low earth orbit (LEO). Drag and gravity effects are successfully used in all of the calculations. The added total result of velocities and altidudes found by these staged rockets are higher than the first single staged case. The advantage of multistage rockets, having same amount of propellant in staged rockets where total velocity will be increased by separating and removing waste from the system weight out of the system. Use of staged rocket system are usefull for increasing the amount of payload and decreasing the cost per unit weight as well.Article Citation - WoS: 5Citation - Scopus: 6Analysis of the Effect of Propellant Temperature on Interior Ballistics Problem(Yildiz Technical Univ, 2018) Evci, C.; Isik, H.This study investigates the effect of conditioning temperature of double base propellants on the interior ballistic parameters such as burning gas temperature, barrel wall temperature, pressure and stresses generated in the barrel. Interior ballistic problem was solved employing experimental, numerical and analytical methods with a thermo-mechanical approach. Double base propellants were conditioned at different temperatures ( 52, 35, 21, 0, -20, -35, -54 degrees C). The maximum pressure in the barrel and projectile muzzle velocity were measured for all the propellants by conducting shooting tests with a special test barrel using 7.62x51 mm NATO ammunition. Vallier-Heydenreich method was employed to determine the transient pressure distribution along the barrel. The temperature of burnt gases was calculated by using Noble-Abel equation. The heat transfer analysis was done using the commercial software ANSYS to get the transient temperature and stress distributions. Temperature distribution through the barrel wall thickness was validated using a FLIR thermal imager. Radial, circumferential and axial stresses and corresponding equivalent Von Misses stresses were determined numerically and analytically. The results of the analytical solution for stress analysis validated the finite element solution of interior ballistic problem. Increasing the initial temperature of the propellant resulted in higher temperature and pressure inside the barrel which in turn increased the stresses in the barrel.Article Theoretical Investigation of Carbon Dioxide Capture by Aqueous Boric Acid Solution: a Termolecular Reaction Mechanism(2018) Kayı, HakanHitherto, boric is suggested and used as a promoter or catalyst for carbondioxide capture in various chemical absorption reactions, such as, absorptionby aqueous potassium carbonate solution to increase mass transfer rate. Butin this study, a single step termolecular reaction mechanism is suggested forthe chemical absorption of carbon dioxide directly by boric acid and water. Thereaction thermochemistry and reaction kinetics for termolecular mechanism areinvestigated by using density functional theory calculations at the B3LYP/6-31G(d)level of theory by taking into account of the implicit solvent effects of water throughthe polarizable continuum model and dispersion corrections. The findings obtainedfrom theoretical calculations indicate that it is possible to capture carbon dioxidewith boric acid in the form of B(OH)2OCOOH.
