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Cogent Engineering Volume 8, 2021 - Issue 1
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MECHANICAL ENGINEERING

Shock and harmonic response analysis of UAV nose landing gear system with air damper

Lovely Son1 Department of Mechanical Engineering, Universitas Sebelas Maret, Surakarta, IndonesiaView further author information
,
Muhammad Surya1 Department of Mechanical Engineering, Universitas Sebelas Maret, Surakarta, IndonesiaView further author information
,
Mulyadi Bur1 Department of Mechanical Engineering, Universitas Sebelas Maret, Surakarta, IndonesiaView further author information
,
Ubaidillah Ubaidillah2 Department of Mechanical Engineering, Universitas Andalas, Padang, IndonesiaCorrespondence[email protected]
ORCID Iconhttps://orcid.org/0000-0002-7190-5849View further author information
ORCID Icon &
Radon Dhelika3 Department of Mechanical Engineering, Universitas Indonesia, Depok, IndonesiaView further author information
|
Duc Pham4 School of Mechanical Engineering, University of Birmingham, Birmingham, UKView further author information
(Reviewing editor)
Article: 1905231 | Received 07 Dec 2020, Accepted 02 Mar 2021, Published online: 15 Apr 2021

Citations (3)

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Read on this site (1)

Jinjin Chen & Caijun Xue. (2023) Design optimisation and experimental verification of a UAV’s landing gear buffer. International Journal of Crashworthiness 0:0, pages 1-10.
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Articles from other publishers (2)

Oğuzhan DAŞ. (2021) Harmonic response analysis of elliptically curved thin plates. International Advanced Researches and Engineering Journal 5:3, pages 426-434.
Crossref
Saeed Rafee Nekoo, Pedro J. Sanchez Cuevas, Jose Angel Acosta, Guillermo Heredia & Anibal Ollero. (2021) Experimental Investigation of Soft-Landing of Quadrotors via Induced Wind Modeling Approach. Experimental Investigation of Soft-Landing of Quadrotors via Induced Wind Modeling Approach.

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