A conceptual method to assess ship-helicopter dynamic interface
Article Properties
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LanguageEnglish
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DOI (url)
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Publication Date2020/01/14
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Indian UGC (journal)
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Refrences17
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Citations2
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Shrish Shukla Department of Applied Mechanics, Indian Institute of Technology Delhi, New Delhi, India ORCID (unauthenticated)
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Sidh N Singh Department of Applied Mechanics, Indian Institute of Technology Delhi, New Delhi, India ORCID (unauthenticated)
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Sawan S Sinha Department of Applied Mechanics, Indian Institute of Technology Delhi, New Delhi, India
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R Vijayakumar Department Ocean Engineering, Indian Institute of Technology Madras, Chennai, India
Abstract
Cite
Shukla, Shrish, et al. “A Conceptual Method to Assess Ship-Helicopter Dynamic Interface”. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 234, no. 5, 2020, pp. 1092-16, https://doi.org/10.1177/0954410019896741.
Shukla, S., Singh, S. N., Sinha, S. S., & Vijayakumar, R. (2020). A conceptual method to assess ship-helicopter dynamic interface. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 234(5), 1092-1116. https://doi.org/10.1177/0954410019896741
Shukla, Shrish, Sidh N Singh, Sawan S Sinha, and R Vijayakumar. “A Conceptual Method to Assess Ship-Helicopter Dynamic Interface”. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 234, no. 5 (2020): 1092-1116. https://doi.org/10.1177/0954410019896741.
Shukla S, Singh SN, Sinha SS, Vijayakumar R. A conceptual method to assess ship-helicopter dynamic interface. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2020;234(5):1092-116.
Journal Categories
Science
Technology
Engineering (General)
Civil engineering (General)
Technology
Mechanical engineering and machinery
Technology
Motor vehicles
Aeronautics
Astronautics
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Refrences
| Title | Journal | Journal Categories | Citations | Publication Date |
|---|---|---|---|---|
Effect of exit Reynolds number on a turbulent round jet | Acta Physica Sinica |
| 11 | 2010 |
| AirDyn: an instrumented model-scale helicopter for measuring unsteady aerodynamic loading in airwakes | Measurement Science and Technology |
| 11 | 2011 |
| Wind Tunnel Testing of a Helicopter Fuselage and Rotor in a Ship Airwake | Journal of the American Helicopter Society | 35 | 2005 | |
| 10.4050/JAHS.49.149 | ||||
| 10.4050/JAHS.47.100 |
Citations
| Title | Journal | Journal Categories | Citations | Publication Date |
|---|---|---|---|---|
| Modeling and Simulation of Ship–Helicopter Dynamic Interface: Method and Application | Archives of Computational Methods in Engineering |
| 3 | 2022 |
| Turbulence characteristics of the ship air-wake with two different topside arrangements and inflow conditions | Ocean Engineering |
| 5 | 2022 |
Citations Analysis
The category
Technology: Engineering (General). Civil engineering (General) 2
is the most commonly referenced area in studies that cite this article. The first research to cite this article was titled Modeling and Simulation of Ship–Helicopter Dynamic Interface: Method and Application and was published in 2022. The most recent citation comes from a 2022 study titled Modeling and Simulation of Ship–Helicopter Dynamic Interface: Method and Application. This article reached its peak citation in 2022, with 2 citations. It has been cited in 2 different journals. Among related journals, the Archives of Computational Methods in Engineering cited this research the most, with 1 citations. The chart below illustrates the annual citation trends for this article.