Abstract The investigation and formal approval of aircraft structures is a necessary step in ensuring initial and continued airworthiness. While component can be predicted using analytical tools, ultimately, the structures must be tested under flight conditions. Substantial over-engineering is unacceptable, due to weight constraints. This chapter therefore describes the main principles of structural approval of aircraft structures, by combination of analysis and test.
First Principles of Structural Approval
Initial Airworthiness ; 113-121
2nd ed. 2018
2018-01-01
9 pages
Article/Chapter (Book)
Electronic Resource
English
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