A Study on the Preliminary Design of Gas Turbine Combustor
가스터빈 연소기 기본형상 결정에 관한 연구
Abstract
The preliminary design and performance test for determining dimensions of gas turbine combustor were investigated. The combustor design program was developed and applied to design our combustor. and detailed design for determining of swirler. dome and liner holes were performed experimentally. The swirler. which govern the combustion characteristics of combustor, was determined
Keywords