Design Of Next Generation Civil And Military Aircraft With Ultra-high Bypass Engine Using Composites, Advanced Materials And Technology

17 pages ID: MCE0290

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Project Details

DepartmentMechanical Engineering
TypeProject
Pages17
Reference StyleYES
FormatMS Word & PDF
Reference No.MCE0290

Abstract

Abstract Indirect combustion noise had not been attracting research in the past, but recent indication seems to prove that it could be a threat in the future if not addressed. Means of reducing this type of noise to a low decibel value was also included. Noise is due to the ingestion of distorted atmospheric turbulence, as the two set of blades rotate in different direction. Open rotor noise is higher since the rotors are fully exposed to oncoming turbulence and lack ducting or a nacelle to attenuate the radiated sound. A thorough review on the technology that can replace conventional turbofan…

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