Dynamic response analysis of the aircraft-snow runway coupling system during taxiing.
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| Title: | Dynamic response analysis of the aircraft-snow runway coupling system during taxiing. |
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| Authors: | Huo, Haifeng1,2 (AUTHOR), Jia, Wentao1 (AUTHOR), Xiao, Enzhao3 (AUTHOR) xiaoenzhao@pric.org.cn, Zhang, Bo4 (AUTHOR), Bao, Xinghua4 (AUTHOR), Li, Tao1 (AUTHOR), Hu, Biao3 (AUTHOR) |
| Source: | International Journal of Pavement Engineering. Dec2025, Vol. 26 Issue 1, p1-15. 15p. |
| Subjects: | ANSYS (Computer system), Acceleration (Mechanics), Strains & stresses (Mechanics), Statistical models, Runways (Aeronautics), Airplanes |
| Abstract: | Compared to traditional runways, compacted snow runways exhibit a reduced surface smoothness and modulus, leading to intensified dynamic responses during aircraft taxiing. This study establishes an aircraft-snow runway interaction model using ANSYS software to quantitatively analyze the effects of the runway wavelength, amplitude, modulus, and aircraft taxiing speed on system dynamics. The results of the study are largely in agreement with the results computed by the ADAMS dynamic analysis software. Specifically, as the wavelength-to-wheelbase ratio increases, the peak acceleration of the landing gear and runway surface decrease rapidly and then gradually stabilise, while the peak runway strain first increases rapidly and then stabilises. As the amplitude increases, the peak acceleration of the landing gear and runway surface continuously increase. Furthermore, the peak vertical strain of the runway decreases. As the runway modulus increases, the peak acceleration of both the landing gear and the runway, as well as the peak runway strain, continuously decrease. With increasing aircraft speed from 2 to 30 m/s, the peak landing gear acceleration rises sharply, while the peak runway acceleration increases correspondingly. The findings of this study offer valuable theoretical guidance for the design and construction of snow-covered runways. [ABSTRACT FROM AUTHOR] |
| Copyright of International Journal of Pavement Engineering is the property of Taylor & Francis Ltd and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 190411240 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Dynamic response analysis of the aircraft-snow runway coupling system during taxiing. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Huo%2C+Haifeng%22">Huo, Haifeng</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Jia%2C+Wentao%22">Jia, Wentao</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Xiao%2C+Enzhao%22">Xiao, Enzhao</searchLink><relatesTo>3</relatesTo> (AUTHOR)<i> xiaoenzhao@pric.org.cn</i><br /><searchLink fieldCode="AR" term="%22Zhang%2C+Bo%22">Zhang, Bo</searchLink><relatesTo>4</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Bao%2C+Xinghua%22">Bao, Xinghua</searchLink><relatesTo>4</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Li%2C+Tao%22">Li, Tao</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Hu%2C+Biao%22">Hu, Biao</searchLink><relatesTo>3</relatesTo> (AUTHOR) – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22International+Journal+of+Pavement+Engineering%22">International Journal of Pavement Engineering</searchLink>. Dec2025, Vol. 26 Issue 1, p1-15. 15p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22ANSYS+%28Computer+system%29%22">ANSYS (Computer system)</searchLink><br /><searchLink fieldCode="DE" term="%22Acceleration+%28Mechanics%29%22">Acceleration (Mechanics)</searchLink><br /><searchLink fieldCode="DE" term="%22Strains+%26+stresses+%28Mechanics%29%22">Strains & stresses (Mechanics)</searchLink><br /><searchLink fieldCode="DE" term="%22Statistical+models%22">Statistical models</searchLink><br /><searchLink fieldCode="DE" term="%22Runways+%28Aeronautics%29%22">Runways (Aeronautics)</searchLink><br /><searchLink fieldCode="DE" term="%22Airplanes%22">Airplanes</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: Compared to traditional runways, compacted snow runways exhibit a reduced surface smoothness and modulus, leading to intensified dynamic responses during aircraft taxiing. This study establishes an aircraft-snow runway interaction model using ANSYS software to quantitatively analyze the effects of the runway wavelength, amplitude, modulus, and aircraft taxiing speed on system dynamics. The results of the study are largely in agreement with the results computed by the ADAMS dynamic analysis software. Specifically, as the wavelength-to-wheelbase ratio increases, the peak acceleration of the landing gear and runway surface decrease rapidly and then gradually stabilise, while the peak runway strain first increases rapidly and then stabilises. As the amplitude increases, the peak acceleration of the landing gear and runway surface continuously increase. Furthermore, the peak vertical strain of the runway decreases. As the runway modulus increases, the peak acceleration of both the landing gear and the runway, as well as the peak runway strain, continuously decrease. With increasing aircraft speed from 2 to 30 m/s, the peak landing gear acceleration rises sharply, while the peak runway acceleration increases correspondingly. The findings of this study offer valuable theoretical guidance for the design and construction of snow-covered runways. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of International Journal of Pavement Engineering is the property of Taylor & Francis Ltd and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
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| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1080/10298436.2025.2470856 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 15 StartPage: 1 Subjects: – SubjectFull: ANSYS (Computer system) Type: general – SubjectFull: Acceleration (Mechanics) Type: general – SubjectFull: Strains & stresses (Mechanics) Type: general – SubjectFull: Statistical models Type: general – SubjectFull: Runways (Aeronautics) Type: general – SubjectFull: Airplanes Type: general Titles: – TitleFull: Dynamic response analysis of the aircraft-snow runway coupling system during taxiing. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Huo, Haifeng – PersonEntity: Name: NameFull: Jia, Wentao – PersonEntity: Name: NameFull: Xiao, Enzhao – PersonEntity: Name: NameFull: Zhang, Bo – PersonEntity: Name: NameFull: Bao, Xinghua – PersonEntity: Name: NameFull: Li, Tao – PersonEntity: Name: NameFull: Hu, Biao IsPartOfRelationships: – BibEntity: Dates: – D: 01 M: 12 Text: Dec2025 Type: published Y: 2025 Identifiers: – Type: issn-print Value: 10298436 Numbering: – Type: volume Value: 26 – Type: issue Value: 1 Titles: – TitleFull: International Journal of Pavement Engineering Type: main |
| ResultId | 1 |