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Aluminum and Carbon Fiber Reinforced Polymer Composite Material Comparative Strength Analysis of a Structural Part in F-16 Fighter Aircraft Landing Gear.

Authors :
KAYA, İlteriş
ÇEVİK, Mehmet
Source :
Journal of Defense Sciences / Savunma Bilmleri Dergisi; kas2023, Vol. 2 Issue 43, p454-472, 19p
Publication Year :
2023

Abstract

<i>Copyright of Journal of Defense Sciences / Savunma Bilmleri Dergisi is the property of Turkish Military Academy Defense Sciences Institute and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)

Details

Language :
English
ISSN :
13036831
Volume :
2
Issue :
43
Database :
Complementary Index
Journal :
Journal of Defense Sciences / Savunma Bilmleri Dergisi
Publication Type :
Academic Journal
Accession number :
174595598
Full Text :
https://doi.org/10.17134/khosbd.1243616