To Estimation of the Parameters of Mathematical Models Characterizing the Strength of an Aircraft after Critical Situations
To Estimation of the Parameters of Mathematical Models Characterizing the Strength of an Aircraft after Critical Situations
- Neue Suche nach: Kostin, V. A.
- Neue Suche nach: Valitova, N. L.
- Neue Suche nach: Gerasimov, A. I.
- Neue Suche nach: Kostin, V. A.
- Neue Suche nach: Valitova, N. L.
- Neue Suche nach: Gerasimov, A. I.
An approach to the study of emergency and failed aircraft objects is considered based on deformation data of the full-scale experiment. The problem of identifying stiffness of the fuselage compartment stringers working in tension–compression under the action of an external load is solved according to the Yu.G. Odinokov model. When minimizing the quality functional, the iterative refinement is applied using sensitivity matrices to find the stiffness of compartment stringers. Numerical results are obtained showing the suitability of the approach for diagnosing the condition of the structure.
Dokumentinformationen
To Estimation of the Parameters of Mathematical Models Characterizing the Strength of an Aircraft after Critical Situations
Russ. Aeronaut.
Russian Aeronautics ; 66 , 3 ; 443-448
2023-08-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Ähnliche Titel
Aircraft Command in Emergency Situations (ACES)
| SAE Technical Papers | 1991
| ELBA - Bundesanstalt für Straßenwesen (BASt) | 2015
Computing Linear Mathematical Models Of Aircraft
| NTRS | 1991
Driving Simulator Studies: The Influence of Vehicle Parameters on Safety in Critical Situations
| SAE Technical Papers | 1974
Predicting Driver Attention in Critical Situations
| British Library Conference Proceedings | 2019