High temperature fatigue testing of gas turbine blades
نویسندگان
چکیده
منابع مشابه
An investigation on fatigue failure of turbine blades of aircraft engines by high cycles fatigue test
Thermal stress, wear and material damage produce effects of high-cycle fatigue failures in aircraft engines. The loading configuration on turbine blades of aircraft engines consists of an axial load. The axial load is the centrifugal force combined with the tensile and compressive loads, caused by the natural vibrations of the blades themselves. Low-cycle fatigue and high-cycle fatigue loading ...
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ژورنال
عنوان ژورنال: Procedia Structural Integrity
سال: 2017
ISSN: 2452-3216
DOI: 10.1016/j.prostr.2017.11.079