Study on Deriving the Buckling Knockdown Factor of a Common Bulkhead Propellant Tank
Author:
Funder
Ministry of Science and ICT
Publisher
The Korean Society of Propulsion Engineers
Subject
General Medicine
Reference18 articles.
1. Peterson, J.P., Seide, P. and Weingarten, V.I., “Buckling of thin-walled circular cylinder,” NASA SP-8007, 1968.
2. Postbuckling Analyses and Derivations of Shell Knockdown Factors for Isogrid-Stiffened Cylinders Under Compressive Force and Internal Pressure
3. Design and Analysis of Subscale and Full-Scale Buckling-Critical Cylinders for Launch Vehicle Technology Development
4. Sub-Scale and Full-Scale Testing of Buckling-Critical Launch Vehicle Shell Structures
5. EN 1993-1-6, “Eurocode 3-Design of steel structures – Part 1-6 : Strength and Stability of Shell Structures,” 2007.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A numerical study on thermal-structural characteristics of cryogenic common bulkhead propellant tanks for various tank lengths and core thicknesses;International Journal of Pressure Vessels and Piping;2024-06
2. A Study on a Modeling Method for Thermal-Structural Coupled Analysis of Cryogenic Common Bulkhead Propellant Tanks;Journal of the Korean Society for Aeronautical & Space Sciences;2023-11-30
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