ABSTRACT Choked flux rates and shock jump relations were calculated both analytically and computationally for a converging-diverging nozzle. High inlet stagnation pressure value with a […]DEVAMINI OKU
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ABSTRACT The cryogenic, vapor-liquid, homogeneous two-phase, inviscid rotational flow through a rocket hirbopump inducer has been solved using three-dimensional and one-dimensional Euler solvers. The […]DEVAMINI OKU
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ABSTRACT Our work focuses on the control of a radial turbojet manufactured by and available at TUSAŞ Engine Industries Inc., equipped with […]DEVAMINI OKU
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ABSTRACT A quasi-three dimensional analysis and design algorithm has been written for the preliminary prediction of the turbomachinery blade shapes. A duct flow […]DEVAMINI OKU
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ABSTRACT The investigation centers on interactions between two hypersonic flows: a nozzle exhausting into an opposing free stream where the angle between the […]DEVAMINI OKU
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ABSTRACT Total Variation Diminishing (TVD) and upwind schemes have been used for the simulation of internal solid rocket motor flows. The […]DEVAMINI OKU
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ABSTRACT The numerical solutions of internal three dimensional Euler flows have been obtained, using a cell vertex finite volume method. The […]DEVAMINI OKU
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ABSTRACT A very fast, loosely-coupled, quasi-three dimensional design algorithm has been written for the preliminary prediction of the turbomachinery blade shapes. A duct flow solver […]DEVAMINI OKU
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ABSTRACT The atrothermodynamic performance of a turbojet engine has been simulated. The method uses the component matching procedure by searching for a […]DEVAMINI OKU
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Cryogenic Homogenous Two-Phase Flows in Choked Laval Nozzles/1999

ABSTRACT The vapor-liquid, two-phase, inviscid, compressible flow in a converging-diverging nozzle has been solYed by high accuracy TVD and Newton-Raphson solvers. Homogeneous speed […]DEVAMINI OKU
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Airfoil Analysis for Horizontal Axis Wind Turbines/1998

ABSTRACT A numerical algorithm has been developed for two dimensional rotating and non-rotating airfoil cross-sections. The steady Euler equations in the rotational plane […]DEVAMINI OKU
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ABSTRACT The numerical solutions of inviscid rotational (Euler) flows were obtained using an explicit hexahedral unstructured cell vertex finite volume method. […]DEVAMINI OKU
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