Conceptual design and optimization of a sustainable and environmentally friendly archetypal helicopter within the selection criteria and limitations

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dc.contributor.authorGunaltili, Enes
dc.contributor.authorEkici, Selcuk
dc.contributor.authorKalkan, Abdullah
dc.contributor.authorGocmen, Faruk Esat
dc.contributor.authorKale, Utku
dc.contributor.authorYilmazoglu, Zeki
dc.contributor.authorKarakoc, T. Hikmet
dc.date.accessioned2023-11-08T11:55:56Z
dc.date.available2023-11-08T11:55:56Z
dc.date.issued2023en_US
dc.departmentRektörlük, Bilişim Teknolojileri Uygulama ve Araştırma Merkezien_US
dc.description.abstractThe design and mission requirements of aero vehicles, which vary on a day-to-day basis, have become major study concerns in the burgeoning aviation sector. In addition to the design and mission criteria that must be met in an aero vehicle design, the designers’ primary goals are to construct original, innovative, environmentally friendly, fuel-efficient, and sustainable designs. In this study, a detailed conceptual design of a helicopter that does not need a notable runway for operation and is limited by mission and design requirements is offered. Within the scope of this research, a competitor analysis study was undertaken in accordance with the defined criteria, and design approaches were chosen based on the outcomes of competitor analysis. In addition, this research, which looks for an environmentally friendly and sustainable design, was developed with the aviation industry’s demands in mind by analyzing the International Helicopter Safety Team’s (IHST) data. As a result of the reports analyzed and considering the causes and consequences of accidents that have happened, the objective of the design research was to achieve a sustainable, ecologically friendly, and fuel-efficient design by reducing the number of accidents and damage. The planning and design processes as a result of this examination are essential as a step towards the helicopter being an original design and in the context of solution methodologies. This archetypal design aims to shed light on helicopter design studies and serve as a roadmap for future research.en_US
dc.identifier.doi10.1016/j.heliyon.2023.e17369en_US
dc.identifier.issue6en_US
dc.identifier.pmid37408911en_US
dc.identifier.scopus2-s2.0-85162855891en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.urihttps://hdl.handle.net/11467/6954
dc.identifier.urihttps://doi.org/10.1016/j.heliyon.2023.e17369
dc.identifier.volume9en_US
dc.identifier.wosWOS:001043006000001en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.indekslendigikaynakPubMeden_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.relation.ispartofHeliyonen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Başka Kurum Yazarıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectHelicopter, Conceptual and sustainable design, Sustainability, Environmentally friendlyen_US
dc.titleConceptual design and optimization of a sustainable and environmentally friendly archetypal helicopter within the selection criteria and limitationsen_US
dc.typeArticleen_US

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