Moving Aerospace Structural Design Practice to a Load and Resistance Factor Approach
| Autor: | Curtis E. Larsen, Ivatury S. Raju |
|---|---|
| Rok vydání: | 2016 |
| Předmět: |
020301 aerospace & aeronautics
Ultimate load Intersection (set theory) Computer science business.industry Calibration (statistics) Probabilistic logic 02 engineering and technology Structural engineering Factor of safety 020303 mechanical engineering & transports 0203 mechanical engineering Factor (programming language) Limit load Aerospace business computer computer.programming_language |
| Zdroj: | 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. |
| DOI: | 10.2514/6.2016-0230 |
| Popis: | Aerospace structures are traditionally designed using the factor of safety (FOS) approach. The limit load on the structure is determined and the structure is then designed for FOS times the limit load - the ultimate load. Probabilistic approaches utilize distributions for loads and strengths. Failures are predicted to occur in the region of intersection of the two distributions. The load and resistance factor design (LRFD) approach judiciously combines these two approaches by intensive calibration studies on loads and strength to result in structures that are efficient and reliable. This paper discusses these three approaches. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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