Abstract: Background: In aircraft applications, engine and nozzle are the two main components which produce high level of noise. The engine noise is predominantly occurred due to piston and otheractuation of subcomponents. Whereas the noise due to nozzle is occurred by mingling of air streams at various temperature and speed. Methods: In this project study, chevron nozzle is studied which is used in aircraft application. And also, theoretical analysis is performed to obtain effective design parameters of chevron nozzle. Hence, Various design of chevron nozzle is modelled by SOLIDWORKS software. The end shape of nozzle is changed such that saw tooth triangular shape is modified by various dimensions and shape. Then, the designed various nozzle is analyzed by ANSYS FLUENT software. In this project, Acoustic power and velocity of those models are calculated and compared for getting efficient model.......
Key Word: Chevron nozzle; CFD analysis; Aircraft engine; Acoustic power
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