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

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

Wang Ziming

Journal of Aeronautical Materials ›› 1987, Vol. 7 ›› Issue (1) : 72-76.

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PDF(4702 KB)

Journal of Aeronautical Materials ›› 1987, Vol. 7 ›› Issue (1) : 72-76.

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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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 1987, 7(1): 72-76

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