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Optimum Ring Stiffened Cylinders Subjected to a Uniform Hydrostatic Pressure* Mechanical and Mathematical Sciences Laboratory, Lockheed Missiles and Space Company
- Format:
- Conference/Event
- Author/Creator:
- Nickell, E. H., author.
- Conference Name:
- National Aerospace Engineering & Manufacturing Meeting
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1962
- Summary:
- Optimum design analyses are presented for ring stiffened cylindrical shells subjected to an external uniform hydrostatic pressure for eight types of ring supported cylinders. Experimental results are included for rectangular ring stiffened shells that demonstrate the validity of the analyses. Optimum configurations are calculated by minimum weight analysis, and sufficient information is presented for design of either optimum or nonoptimum configurations
- Notes:
- Vendor supplied data
- Publisher Number:
- 620362
- Access Restriction:
- Restricted for use by site license
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