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飞机座舱盖玻璃成型残余应力测定-双折射主切片退火法
({{custom_author.role_cn}}), {{javascript:window.custom_author_cn_index++;}}DETERMINATION OF RESIDUAL STRESS CAUSED BY FORMING IN TRANSPARENT AIRPLANE CA NOPY-AMETHOD USI NG BIREFRI NGE NCEFIRST SLICE BEFORE AND AFTER ANNEALING TO DETERMINE RESIDUAL STRESS
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