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مکانیک::
شرود خارجی
The maximum tensile stress is about 210 MPa, which is generated at either the leading or trail- ing edge portions on the inner surface of the outer shroud.
The temperature difference between the shroud and airfoil sec- tions results in the generation of thermal stresses that tend to be maximized at either the leading edge or the trailing edge on the inner surface of the outer shroud.
The ceramic temperatures are measured at outer shroud and at 50 and 95 percent vane heights at the leading edge portion of the airfoil sec- tion.
Outer shroud 95% height 50% height
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