Simulations and Tests of a KRET Aerospace Penetrator
This manuscript presents the simulation tests of an aerospace penetrator conducted to check the device’s validity and functionality. For this work, the numerical model was created on the basis of engineering data, the laboratory model of the tube reluctance actuator was created on the basis of the n...
| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2020-06-01
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| Series: | Energies |
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| Online Access: | https://www.mdpi.com/1996-1073/13/12/3291 |
| _version_ | 1827714183564623872 |
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| author | Krzysztof Bieńkowski Łukasz Kolimas Sebastian Łapczyński Michał Drogosz Michał Szulborski Łukasz Wiśniewski Bartosz Kędziora Łukasz Kozarek |
| author_facet | Krzysztof Bieńkowski Łukasz Kolimas Sebastian Łapczyński Michał Drogosz Michał Szulborski Łukasz Wiśniewski Bartosz Kędziora Łukasz Kozarek |
| author_sort | Krzysztof Bieńkowski |
| collection | DOAJ |
| description | This manuscript presents the simulation tests of an aerospace penetrator conducted to check the device’s validity and functionality. For this work, the numerical model was created on the basis of engineering data, the laboratory model of the tube reluctance actuator was created on the basis of the numerical model, and a set of simulations were executed on the basis of both presented. Moreover, the mathematical model was supplemented by precise boundary conditions. The main goal was the analysis of the introduced device’s properties by comparing them to experimental values. Three different variants were taken into account to check the construction functionality and to study the most important parameters, e.g., the hammer displacement, hammer velocity, eddy currents and overall electromagnetic properties of the penetrator’s hammer displacement. The high-end values of the applied components were derived on the basis of the results and are presented in the summary of the concluded work. An overall method for checking the validity of the penetrator was proposed, which is cost and time effective. The model used was not limited in the representation of physical phenomena. |
| first_indexed | 2024-03-10T18:52:11Z |
| format | Article |
| id | doaj.art-42d265c004fc41b59cf8c5a486fd70b0 |
| institution | Directory Open Access Journal |
| issn | 1996-1073 |
| language | English |
| last_indexed | 2024-03-10T18:52:11Z |
| publishDate | 2020-06-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Energies |
| spelling | doaj.art-42d265c004fc41b59cf8c5a486fd70b02023-11-20T05:02:11ZengMDPI AGEnergies1996-10732020-06-011312329110.3390/en13123291Simulations and Tests of a KRET Aerospace PenetratorKrzysztof Bieńkowski0Łukasz Kolimas1Sebastian Łapczyński2Michał Drogosz3Michał Szulborski4Łukasz Wiśniewski5Bartosz Kędziora6Łukasz Kozarek7Astronika Sp. z o.o., ul. Bartycka 18, 00-716 Warsaw, PolandInstitute of Electrical Power Engineering, Warsaw University of Technology, 00-662 Warsaw, PolandInstitute of Electrical Power Engineering, Warsaw University of Technology, 00-662 Warsaw, PolandSyderal Sp. z o.o., ul. Trzy Lipy 3, 80-172 Gdansk, PolandInstitute of Electrical Power Engineering, Warsaw University of Technology, 00-662 Warsaw, PolandAstronika Sp. z o.o., ul. Bartycka 18, 00-716 Warsaw, PolandAstronika Sp. z o.o., ul. Bartycka 18, 00-716 Warsaw, PolandInstitute of Electrical Power Engineering, Warsaw University of Technology, 00-662 Warsaw, PolandThis manuscript presents the simulation tests of an aerospace penetrator conducted to check the device’s validity and functionality. For this work, the numerical model was created on the basis of engineering data, the laboratory model of the tube reluctance actuator was created on the basis of the numerical model, and a set of simulations were executed on the basis of both presented. Moreover, the mathematical model was supplemented by precise boundary conditions. The main goal was the analysis of the introduced device’s properties by comparing them to experimental values. Three different variants were taken into account to check the construction functionality and to study the most important parameters, e.g., the hammer displacement, hammer velocity, eddy currents and overall electromagnetic properties of the penetrator’s hammer displacement. The high-end values of the applied components were derived on the basis of the results and are presented in the summary of the concluded work. An overall method for checking the validity of the penetrator was proposed, which is cost and time effective. The model used was not limited in the representation of physical phenomena.https://www.mdpi.com/1996-1073/13/12/3291reluctance actuatoraerospace penetratorFEMsimulationmole penetratorKRET |
| spellingShingle | Krzysztof Bieńkowski Łukasz Kolimas Sebastian Łapczyński Michał Drogosz Michał Szulborski Łukasz Wiśniewski Bartosz Kędziora Łukasz Kozarek Simulations and Tests of a KRET Aerospace Penetrator Energies reluctance actuator aerospace penetrator FEM simulation mole penetrator KRET |
| title | Simulations and Tests of a KRET Aerospace Penetrator |
| title_full | Simulations and Tests of a KRET Aerospace Penetrator |
| title_fullStr | Simulations and Tests of a KRET Aerospace Penetrator |
| title_full_unstemmed | Simulations and Tests of a KRET Aerospace Penetrator |
| title_short | Simulations and Tests of a KRET Aerospace Penetrator |
| title_sort | simulations and tests of a kret aerospace penetrator |
| topic | reluctance actuator aerospace penetrator FEM simulation mole penetrator KRET |
| url | https://www.mdpi.com/1996-1073/13/12/3291 |
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