DETERMINATION OF RESIDUAL STRESS CAUSED BY FORMING IN TRANSPARENT AIRPLANE CANOPIES——A GRAPHIC METHOD BY MEANS OF THE BIREFRINGENCE IN THE FIRST SLICE

DETERMINATION OF RESIDUAL STRESS CAUSED BY FORMING IN TRANSPARENT AIRPLANE CANOPIES——A GRAPHIC METHOD BY MEANS OF THE BIREFRINGENCE IN THE FIRST SLICE

Wang Ziming

Journal of Aeronautical Materials ›› 1989, Vol. 9 ›› Issue (1) : 31-39,30.

PDF(645 KB)

PDF(645 KB)

Journal of Aeronautical Materials ›› 1989, Vol. 9 ›› Issue (1) : 31-39,30.

DETERMINATION OF RESIDUAL STRESS CAUSED BY FORMING IN TRANSPARENT AIRPLANE CANOPIES——A GRAPHIC METHOD BY MEANS OF THE BIREFRINGENCE IN THE FIRST SLICE

{{article.zuoZhe_EN}}

Author information +

History +

HeighLight

{{article.keyPoints_en}}

Abstract

{{article.zhaiyao_en}}

Key words

QR code of this article

Cite this article

Download Citations

{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 1989, 9(1): 31-39,30

References

List( Publishing order | Descend order by publishing year | Descend order by cited within ) Chart analysis

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}

{{article.copyrightLicense_en}}

PDF(645 KB)

Accesses

Citation

Detail

Sections

Recommended

/

〈

〉