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    Thermal Analysis of Regenerative Cooling in Liquid Rocket Engines

    , M.Sc. Thesis Sharif University of Technology Azizi, Mahdi (Author) ; Kebriaei, Azadeh (Supervisor)
    Abstract
    In this thesis to simulate the behavior of liquid engine Thrust chamber of hot gas from a quasi one dimensional code used when the effects of the heat transfer and friction in those terma. As well as during the regenerative channel is simulated by considering the equation’s of continuity, momentum and energy for one dimensional, effects of increase temperature, pressure drop, change the density of coolant flow resulting from the warming which is visible along the way to increase the accuracy of calculation of the thermal flux output of the engine, use a suitable model for unclear boiling in consideration of heat transfer coefficient used coolant flow it has been. As well as coupling of heat... 

    Investigation of Flow Formed by two Impinging Jets

    , M.Sc. Thesis Sharif University of Technology Dolatkhahi, Hamed (Author) ; Kebriaei, Azadeh (Supervisor)
    Abstract
    Due to importance of designing geometry and working condition of injector it is necessary that by testing cold flow, we gain better understanding of atomization characteristics and in particular initial atomization close to injector which defines the spray characteristics. Up to today experimental measurements in the high density zone close to injector has been difficult to to optical limitations and also analytical solutions of atomization process is limited due to complexity and highly nonlinear equations. Numerical solutions are also under development and researchers have recently done researches and simulations. In this field the modeling of liquid sheet collapse has challenged numerical... 

    Implementation of Pressure Sensitive Paint (PSP)Method for Pressure Distribution Measurement

    , M.Sc. Thesis Sharif University of Technology Ahmadi, Farhad (Author) ; Kebriaei, Azadeh (Supervisor)
    Abstract
    Quantitative measurement of pressure on surfaces in wind tunnels and flight tests is essential to understand the aerodynamic performance of flying vehicles. Pressure data are also essential for validation and verification of computational fluid dynamics codes. One of the relatively new methods of measuring pressure distribution on aerodynamic surfaces is the method of pressure sensitive paint (PSP). The PSP method is an optical technique that can measure the pressure distribution on the surface without using common pressure sensors or transducers, with greater spatial resolution and lower cost. This method has a unique ability for non-contact (non-interfering) measurements. In this method,... 

    Implementation of Local Chemiluminescence Method on Flame

    , M.Sc. Thesis Sharif University of Technology Reyhani, Anahita (Author) ; Kebriaei, Azadeh (Supervisor)
    Abstract
    In the present work, the local Chemiluminescence method has been implemented on a laminar premixed propane-air flame. The goal of this work is to achieve a system capable of measuring the intensity of Chemiluminescent radiations of CH* and OH* radicals locally and with high spatial and temporal accuracy. For this purpose, a setup has been designed and developed. In order to achieve high spatial accuracy for local measurements, a Cassegrain lens has been designed and built, which has the ability to collect light from a cylindrical control volume with a cross-sectional diameter of 58 μm and a depth of 3.4 mm. An optical system for dividing and filtering light based on wavelength has also been...