ÖZET Aerodinamik rotor ve hazne geometrisi ve termodinamik çevrimi ile özgün bir yapya sahip olan yeni bir turbo döngüsel motorun yanma […]DEVAMINI OKU
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Engine Design Model for Seperate Flow Turbofan Engine/2013

ABSTRACT The first step in Engine Design for an airframe is being the on-design cycle analysis. The results of this analysis […]DEVAMINI OKU
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EXTENDED ABSTRACT Thermal efficiency of a gas turbine engine is highly dependent on the turbine inlet gas temperature. Increasing the […]DEVAMINI OKU
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ABSTRACT There are different characters of air flow in a conventional gas turbine blade cooling channel. These flow characters; including high streamline […]DEVAMINI OKU
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Adaptive Unstructured Grid Applications for Multi-element Airfoils/2001

ABSTRACT Unstructured grids are generated for multi-element airfoils and the corresponding Euler and Navier- Stokes flow solutions are obtained around NLR7301 and NLHP […]DEVAMINI OKU
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ABSTRACT A new methodology is developed to Ž find the optimal aerodynamic performance of a turbine cascade.A boundary layer coupled Euler […]DEVAMINI OKU
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Unmanned Air Vehicle Turbo Rotary Engine Preliminary Component Tests/2008

ABSTRACT A 1.5 kW rotary vane engine is designed to power small unmanned air vehicles. This external combustion heat engine is […]DEVAMINI OKU
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ABSTRACT For a maximum power output, the wind turbines should be selected according to the wind characteristics of the terrain. The most […]DEVAMINI OKU
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ABSTRACT Weighted Essentially Non-Oscillatory schemes are high order accurate schemes designed for problems with piecewise smooth solutions containing discontinuities. Those schemes are mainly […]DEVAMINI OKU
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Turbo-Rotary Compound Engine (TRCE) and Novel Thermodynamic Cycle/2005

ABTRACT The present paper proposes a new turbo-rotary compound engine (TRCE) and an associated novel thermodynamic cycle. In this engine, […]DEVAMINI OKU
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ÖZET Bu çalışmada gaz türbinlerinin döngüsel komponentlerinin performans haritalarının çıkarılması öngörülmüştür. Bu haritalarının elde edilmesi için oluşturulan modellerde kompresör ve türbin kademe özelliklerinin genelleştirildiği […]DEVAMINI OKU
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Uçak Motor ve Gaz Türbinlerinde Performans ve Verim Artışları/2004

ÖZET Uçak motor ve gaz türbinlerinin güçlerini ve termik verimlerini bugünlerde bulunduğu seviyelerden daha yukarı çıkarmak mümkündür. Gaz türbin motor grubu ile döngüsel […]DEVAMINI OKU
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