1) wing crack
翼裂隙
1.
A new fracture pattern is observed where an anti-wing crack(its growth direction is opposite to that of wing crack)is induced at a distance away from the flaw tip in the region of compression stress zone.
试验结果表明:预制裂隙的破裂模式是以一种新的方式——反翼裂隙(其扩展方向是与翼裂隙方向相反的)模式为主的,且新生裂隙的起裂位置并不在预制裂隙的端部。
2) anti-wing crack
反翼裂隙
1.
A new fracture pattern is observed where an anti-wing crack(its growth direction is opposite to that of wing crack)is induced at a distance away from the flaw tip in the region of compression stress zone.
试验结果表明:预制裂隙的破裂模式是以一种新的方式——反翼裂隙(其扩展方向是与翼裂隙方向相反的)模式为主的,且新生裂隙的起裂位置并不在预制裂隙的端部。
3) wing crack
翼裂纹
1.
The experimental results show that wrapping wing cracks individually initiate and grow from every pre-existing flaw end at the beginning of fractures.
试验结果表明:试验早期阶段,各裂隙在端部均以包裹式翼裂纹起裂,并独立地扩展。
4) anti-wing crack
反翼裂纹
5) ala nasi cleft
鼻翼裂
1.
Multiple-deformities with congenital cleft lip, ala nasi cleft, face horizontal cleft, accessory ear and inguinal hernia:A case report;
罕见先天性唇裂、鼻翼裂、面横裂、附耳等多发畸形伴斜疝1例
6) initiation angle of wing crack
翼裂纹起裂角
补充资料：变后掠翼飞机(见后掠翼飞机)
变后掠翼飞机(见后掠翼飞机)
swing-wing aircraft
bianhoul位eyi feiii变后掠翼飞机(swing一wing aircran)见后掠翼飞机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。