Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts
The goal of this paper is to investigate the possible directions of some specified methods for aeronautical and aerospace material and structure effectiveness modeling and optimization. Multioptionality hybrid function uncertainty conditional optimization doctrine application is supposed to be imple...
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| Format: | Article |
| Language: | English |
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Wiley
2018-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2018/4126085 |
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| _version_ | 1832555480645369856 |
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| author | Andriy Viktorovich Goncharenko |
| author_facet | Andriy Viktorovich Goncharenko |
| author_sort | Andriy Viktorovich Goncharenko |
| collection | DOAJ |
| description | The goal of this paper is to investigate the possible directions of some specified methods for aeronautical and aerospace material and structure effectiveness modeling and optimization. Multioptionality hybrid function uncertainty conditional optimization doctrine application is supposed to be implemented for a degrading failure problem optimal solution determination. The optimal solution is assumed to deliver the maximum value to the probability of damage but not the failure state of the studied material behavior. The principal supposition is that there should be some certain objectively existing value extremized in the conditions of the hybrid optional function uncertainty. There is a scientific proof for the choice of a good maintenance optimal periodicity method that fits the customer’s needs, taking into account the effectiveness functions pertaining to the options. The described doctrine allows obtaining the objectively existing optimal values not with the help of a probabilistic but rather with a multioptimal concept. The subjective entropy maximum principle is the other paradigm concept involved in the considered problem solution, which is an equivalent for the uncertainty conditional optimization at the optimal hybrid function distribution determination. By applying simplified, however possible, models and expressions for effectiveness, plausible results are obtained and illustrated in diagrams visualizing the situation and allowing for the selection of a good choice. The ideas of the required material method choice optimization with respect to only two simple parameters, nevertheless, develop numerous particular combinations. Moreover, an increase in the number of parameters and further complication of the problem setting will not change the principle of the problem solution. |
| format | Article |
| id | doaj-art-9484a58239c340b3a912f51d48f9c455 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2018-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-9484a58239c340b3a912f51d48f9c4552025-02-03T05:48:12ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742018-01-01201810.1155/2018/41260854126085Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical ConceptsAndriy Viktorovich Goncharenko0Aircraft Airworthiness Retaining Department, Educational and Research Airspace Institute, National Aviation University, 1 Kosmonavta Komarova Avenue, Kyiv 03058, UkraineThe goal of this paper is to investigate the possible directions of some specified methods for aeronautical and aerospace material and structure effectiveness modeling and optimization. Multioptionality hybrid function uncertainty conditional optimization doctrine application is supposed to be implemented for a degrading failure problem optimal solution determination. The optimal solution is assumed to deliver the maximum value to the probability of damage but not the failure state of the studied material behavior. The principal supposition is that there should be some certain objectively existing value extremized in the conditions of the hybrid optional function uncertainty. There is a scientific proof for the choice of a good maintenance optimal periodicity method that fits the customer’s needs, taking into account the effectiveness functions pertaining to the options. The described doctrine allows obtaining the objectively existing optimal values not with the help of a probabilistic but rather with a multioptimal concept. The subjective entropy maximum principle is the other paradigm concept involved in the considered problem solution, which is an equivalent for the uncertainty conditional optimization at the optimal hybrid function distribution determination. By applying simplified, however possible, models and expressions for effectiveness, plausible results are obtained and illustrated in diagrams visualizing the situation and allowing for the selection of a good choice. The ideas of the required material method choice optimization with respect to only two simple parameters, nevertheless, develop numerous particular combinations. Moreover, an increase in the number of parameters and further complication of the problem setting will not change the principle of the problem solution.http://dx.doi.org/10.1155/2018/4126085 |
| spellingShingle | Andriy Viktorovich Goncharenko Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts International Journal of Aerospace Engineering |
| title | Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts |
| title_full | Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts |
| title_fullStr | Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts |
| title_full_unstemmed | Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts |
| title_short | Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts |
| title_sort | aeronautical and aerospace material and structural damages to failures theoretical concepts |
| url | http://dx.doi.org/10.1155/2018/4126085 |
| work_keys_str_mv | AT andriyviktorovichgoncharenko aeronauticalandaerospacematerialandstructuraldamagestofailurestheoreticalconcepts |