The structural integrity evaluation of the aero structures and components is of paramount importance not just to validate the design and manufacturing processes, but it is also mandatory to prove the satisfactory compliance of design objectives laid down with respect to the performance and functioning. The paper depicts the methods employed for simulating the bird-strikes on the aero structures (of both military and civilian aircrafts) in the state-of-the-art test facility developed for conducting such tests along with some test cases and conceptualizing a new technique for the high (linear) speed measurement of the bird.
Methods of Simulation of Bird-Strikes on Critical Aero Structures with Some Test Cases and Conceptualization of an Alternative Technique for the High-Speed Measurement
Lect.Notes Mechanical Engineering
2020-08-01
16 pages
Article/Chapter (Book)
Electronic Resource
English
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