Strength Analysis of an Aircraft Sandwich Structure with a Honeycomb Core: Theoretical and Experimental Approaches
In this paper, the strength of aircraft sandwich structure with honeycombcore under bending load was evaluated theoretically and experimentallybased on failure mode maps. A failure mode map for the loading underthree-point bending was constructed theoretically to specify the failuremodes and corresp...
Main Authors: | Sadiq E. Sadiq, Muhsin J. Jweeg, Sadeq H. Bakhy |
---|---|
Format: | Article |
Language: | English |
Published: |
Unviversity of Technology- Iraq
2021-01-01
|
Series: | Engineering and Technology Journal |
Subjects: | |
Online Access: | https://etj.uotechnology.edu.iq/article_168100_87393cf58365f767158ae9c6472b567c.pdf |
Similar Items
-
Tolerance Modelling of Vibrations of a Sandwich Plate with Honeycomb Core
by: Jakub Marczak
Published: (2022-10-01) -
EFFECT OF CORE HEIGHT ON GENERAL STABILITY OF HONEYCOMB SANDWICH STRUCTURE
by: JIN Di, et al.
Published: (2017-01-01) -
The response of honeycomb core sandwich panels, with aluminum and composite face sheets, to blast loading/
by: Langdon, G. S., et al. -
Composite honeycomb core sandwich plate with facesheet indentation model subjected to low-velocity impact /
by: Siti Hasyyati Drahman, 1989- , author, et al.
Published: (2015) -
Investigation of flexural strength of jute fiber based circular type honeycomb sandwich panel: An experimental and numerical approach
by: Asif Hosen, et al.
Published: (2023-09-01)