Galchenko S. The method of in-flight diagnostic of the state of external surface of airplane's wing

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0407U004728

Thesis Registration Form

0407U004728.pdf

Applicant for

Specialization

  • 05.22.20 - Експлуатація та ремонт засобів транспорту

31-10-2007

Specialized Academic Board

Д 26.062.03

National Aviation University

Essay

The developed method helps to determinate moment, place and degree of sudden damage of external surface of airplane's wing in flight via indirect registration of changes of local forces and moments in the places of origin of sudden damage and also determinates wing's damaged area using matrix of gravimetric coefficients and theory of the thermal field. Proposed method of identification and classification of the damage types with applying the Bayesian theory of neural networks, as well as designed the structure of the neurounclear regulator which takes into account the sudden damages of wing's surface.

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Files

aref.doc

dis1.doc

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