Analysing temperature distributions in turbine first-stage rotor blades of a helicopter turboshaft engine
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This article presents a numerical investigation focusing on the temperature distribution of first-stage turbine rotor blades that do not feature internal cooling channels. The results indicate the regions of peak temperatures and evaluate rotor blade strength.
Nội dung trích xuất từ tài liệu:
Analysing temperature distributions in turbine first-stage rotor blades of a helicopter turboshaft engine
Nội dung trích xuất từ tài liệu:
Analysing temperature distributions in turbine first-stage rotor blades of a helicopter turboshaft engine
Tìm kiếm theo từ khóa liên quan:
Science and transport technology High-pressure turbine Rotor blade Mechanical properties Analysing temperature distributionsTài liệu liên quan:
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