Research and strength analysis of hoop bending test of composite fuselage integral frame
As the main bearing structure of civil aircraft, the fuselage frame is of great significance to the weight of the aircraft.A hoop bending test is carried out on the composite fuselage curved panels with C-type and Z-type integral frames to study the failure mode and load-bearing capacity of the inte...
Main Authors: | , , |
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Format: | Article |
Language: | zho |
Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2023-02-01
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Series: | Hangkong gongcheng jinzhan |
Subjects: | |
Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2022037 |