The Behaviour Of Cylindrical Corrugated Core Sandwich Stuctures Under The Combination of Quasi-Static Axial Compressive and Internal Pressure Loadings-Reference-Cited by-同舟云学术

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The Behaviour Of Cylindrical Corrugated Core Sandwich Stuctures Under The Combination of Quasi-Static Axial Compressive and Internal Pressure Loadings

Published:2024 Issue: Volume: Page:
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Author:

Bakhtari Jorghy Sultan,Hadi Bambang Kismono,Kusni Muhammad,Widagdo Djarot

Publisher

Elsevier BV

Reference22 articles.

1. Weight Comparisons of Optimized Stiffened, Unstiffened, and Sandwich Cylindrical Shells;B L Agarwal;Journal of Aircraft,1977

2. Buckling of cylindrical sandwich shells with metal foam cores;J W Hutchinson;International Journal of Solids and Structures,2000

3. On the minimum weights of compression structures;B Budiansky;International Journal of Solids and Structures,1999

4. Buckling of orthotropic sandwich cylinders under axial compression and bending;C D Reese;Journal of Aircraft,1974

5. Buckling of Sandwich Cylinders Under Axial Compression;F K Teichmann;Journal of the Aeronautical Sciences,1951

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