Study on crack propagation behaviors of aircraft internal pressure panels with longitudinal cracks
Crack growth analysis of aircraft fuselage panels is one of the important tasks of aircraft damage tolerance design. In this paper, the crack growth behavior and residual strength characteristics of the internal pressure panel of the aircraft fuselage with longitudinal cracks were analyzed from two...
Saved in:
Main Authors: | QIN JianBo, WANG Feng, LÜ Pin, HOU Cheng, FAN XueLing |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2024-06-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2024.03.006 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Damage tolerance analysis of aircraft reinforced panels
by: A. Pirondi, et al.
Published: (2011-04-01) -
DAMAGE TOLERANCE EXPERIMENT AND ANALYSIS OF STIFFENED FUSELAGE PANEL WITH LONGITUDINAL CRACK
by: CHEN An, et al.
Published: (2017-01-01) -
RESEARCH ON THE FATIGUE CRACK PROPAGATION OF AIRCRAFT FUSELAGE SKIN UNDER UNIFORM PRESSURIZED LOAD (MT)
by: LIU LiPing, et al.
Published: (2023-01-01) -
ANALYSIS AND APPLICATION OF THREE-DIMENSIONAL CRACK GROWTH BASED ON FRANC3D
by: AI ShuMin, et al.
Published: (2018-01-01) -
RESEACH OF THREE-DIMENSIONAL CRACK GROWTH BASED ON DISK OF TURBO-SHAFT ENGINE
by: AI ShuMin, et al.
Published: (2018-01-01)