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- Title
Free vibration analysis of a discretized aircraft with an integrated biodynamic pilot model - modal approach.
- Authors
Gowtham, C. Hari; Balila, Adarsha; Ankush, B. N.; Chandrashekara, C. V.
- Abstract
This work deals with the formulation of mathematical model for a discretized aircraft with combined seated biodynamic pilot model. The developed model provides scope for exploring the dynamic characteristics of the aircraft system and pilot under various runway operations and landing impacts. Modal analysis approach is used to obtain the free vibration characteristics of multi degrees-of-freedom system. The obtained results like natural frequencies, mode shapes and undamped response curves are reported.
- Subjects
MODE shapes; MODAL analysis; MODEL airplanes; FREE vibration; MATHEMATICAL models
- Publication
Vibroengineering Procedia, 2020, Vol 30, p133
- ISSN
2345-0533
- Publication type
Article
- DOI
10.21595/vp.2020.21394