飞机座舱盖玻璃成型残余应力测定-双折射主切片退火法
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
{{custom_ref.label}} |
{{custom_citation.content}}
{{custom_citation.annotation}}
|
/
〈 | 〉 |