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Buckling Of Circular Cylindrical Shells Under Dynamically Applied Axial Loads by James Douglas Tulk
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1NASA Technical Reports Server (NTRS) 19730003200: Buckling Of Circular Cylindrical Shells Under Dynamically Applied Axial Loads
By NASA Technical Reports Server (NTRS)
A theoretical and experimental study was made of the buckling characteristics of perfect and imperfect circular cylindrical shells subjected to dynamic axial loading. Experimental data included dynamic buckling loads (124 data points), high speed photographs of buckling mode shapes and observations of the dynamic stability of shells subjected to rapidly applied sub-critical loads. A mathematical model was developed to describe the dynamic behavior of perfect and imperfect shells. This model was based on the Donnell-Von Karman compatibility and equilibrium equations and had a wall deflection function incorporating five separate modes of deflection. Close agreement between theory and experiment was found for both dynamic buckling strength and buckling mode shapes.
“NASA Technical Reports Server (NTRS) 19730003200: Buckling Of Circular Cylindrical Shells Under Dynamically Applied Axial Loads” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19730003200: Buckling Of Circular Cylindrical Shells Under Dynamically Applied Axial Loads
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19730003200: Buckling Of Circular Cylindrical Shells Under Dynamically Applied Axial Loads” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - BUCKLING - CIRCULAR SHELLS - COMPRESSION LOADS - STRUCTURAL FAILURE - DESTRUCTIVE TESTS - MATHEMATICAL MODELS - SHELL STABILITY - STRESS ANALYSIS - Tulk, J. D.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19730003200
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 110.92 Mbs, the file-s for this book were downloaded 106 times, the file-s went public at Sat Jul 09 2016.
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