Relevant bibliographies by topics / Spiroid winglets

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  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Spiroid winglets'

Author: Grafiati
Published: 4 June 2025
Last updated: 1 August 2025

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Journal articles on the topic "Spiroid winglets"

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Rodríguez-Sevillano, Ángel Antonio, Rafael Bardera-Mora, Alejandra López-Cuervo-Alcaraz, et al. "Automation of Winglet Wings Geometry Generation for Its Application in TORNADO." Algorithms 16, no. 9 (2023): 439. http://dx.doi.org/10.3390/a16090439.

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The paper outlines an algorithm for the rapid aerodynamic evaluation of winglet geometries using the TORNADO Vortex Lattice Method. It is a very useful tool to obtain a first approximation of the aerodynamic properties and for performing an optimization of the geometry design. The TORNADO tool is used to systematically calculate the aerodynamic characteristics of various wings with wingtip devices. The fast response of the aerodynamic models allows obtaining a set of results in a remarkably short time. Therefore, the development of an algorithm to generate wing geometries with great ease and c
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Abd, Dalya Adnan, and Anmar Hamed Ali. "Aerodynamic Characteristics Comparison between Spiroid and Blended Winglets." Journal of Engineering 26, no. 4 (2020): 33–46. http://dx.doi.org/10.31026/j.eng.2020.04.03.

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Mostafa, Suhail, Shyam Bose, Archana Nair, et al. "A parametric investigation of non-circular spiroid winglets." EPJ Web of Conferences 67 (2014): 02077. http://dx.doi.org/10.1051/epjconf/20146702077.

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Guerrero, Joel E., Dario Maestro, and Alessandro Bottaro. "Biomimetic spiroid winglets for lift and drag control." Comptes Rendus Mécanique 340, no. 1-2 (2012): 67–80. http://dx.doi.org/10.1016/j.crme.2011.11.007.

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Viktor, Popov, Loginov Vasiliy, Ukrainets Yevgen, Shmyrov Volodymyr, Steshenko Petro, and Hlushchenko Pavlo. "IMPROVING AIRCRAFT FUEL EFFICIENCY BY USING THE ADAPTIVE WING AND WINGLETS." Eastern-European Journal of Enterprise Technologies 2, no. 1 (104) (2020): 51–59. https://doi.org/10.15587/1729-4061.2020.200664.

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Improving the aircraft’s fuel efficiency is one of the main requirements for prospective and modernized aircraft. This paper reports the assessment of change in aerodynamic quality resulting in the improved fuel efficiency of a long-range aircraft when using promising means to enhance aerodynamic quality. These means include the abandonment of the mechanization of wing edges and conventional controls through the use of an adaptive wing, the artificial laminarization of the flow around the elements of a glider, the application of winglets. The abandonment of conventional wing controls and
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Sormin, Muhammad Randy, and Rosyida Permatasari. "ANALISIS SPIROID WINGLET PADA PESAWAT SUBSONIC DENGAN VARIASI SUDUT SERANG TERHADAP KONSUMSI BAHAN BAKAR MENGGUNAKAN METODE COMPUTATIONAL FLUID DYNAMIC." JURNAL PENELITIAN DAN KARYA ILMIAH LEMBAGA PENELITIAN UNIVERSITAS TRISAKTI 5, no. 1 (2020): 1–7. http://dx.doi.org/10.25105/pdk.v5i1.6414.

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Winglet merupakan komponen aerodinamika yang digunakan pada sayap pesawat untuk mengurangi induced drag yang terjadi pada sayap pesawat saat terbang. Induced drag merupakan gaya aerodinamik yang terjadi akibat fenomena vortex pada sayap pesawat dikarenakan adanya perpindahan aliran udara pada lapisan batas dari bagian bawah sayap yang bertekanan tinggi ke bagian atas yang bertekanan rendah. Pada penelitian ini dibahas pengaruh bentuk winglet, yaitu spiroid winglet, pada pesawat subsonic yang akan mengurangi induced drag yang terjadi Penelitian dilakukan dengan melakukan simulasi menggunakan me
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Fathi, Behrouz. "Applying Spiroid Winglet on The Tip of NREL 5 MW Offshore Wind Turbine’s Blade to Investigate Vortex Effects." E3S Web of Conferences 197 (2020): 08004. http://dx.doi.org/10.1051/e3sconf/202019708004.

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The present research describes the numerical investigation of the aerodynamics around a wind turbine blade with a winglet using Computational Fluid Dynamics, CFD. In this project our goal is to applying spiroid winglet to examine of the vortex effects on the tip of wind turbine’s blade known as “NREL offshore 5-MW baseline wind turbine”. At present this method has not yet been implemented in the wind energy sector, in particular because their production still involves excessive costs, compared to the benefits obtainable in terms of wind energy field. A spiroid winglet was investigated with dif
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PILLAI, T. GOTTFRIED. "Knightjonesia, a new genus (Polychaeta: Spirorbidae) with a winged opercular peduncle, and its taxonomy." Zootaxa 2059, no. 1 (2009): 46–50. http://dx.doi.org/10.11646/zootaxa.2059.1.4.

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It had hitherto been assumed in publications on serpulimorph systematics that spirorbids are characterized by an operculum borne on a wingless peduncle. However, while examining various spirorbid collections in the Natural History Museum, London, it was found that the type specimens of Helicosiphon platyspira Knight-Jones, 1978 possess a winged opercular peduncle, a character that had hitherto been used to distinguish between other serpulimorph genera. Accordingly, Helicosiphon platyspira is transferred to a new genus, Knightjonesia, in which the opercular peduncle is winged, in contrast with
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Dissertations / Theses on the topic "Spiroid winglets"

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Kuei-Wen, Lien. "Numerical Investigation of Aerodynamic Efficiency for Spiroid Winglet with Blowing." 2006. http://www.cetd.com.tw/ec/thesisdetail.aspx?etdun=U0002-2808200609354900.

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Lien, Kuei-Wen, and 連魁文. "Numerical Investigation of Aerodynamic Efficiency for Spiroid Winglet with Blowing." Thesis, 2004. http://ndltd.ncl.edu.tw/handle/83397639677635417729.

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碩士<br>淡江大學<br>航空太空工程學系碩士班<br>94<br>Since 1976 Richard T. Whitcomb has shown that the efficiency of the aircraft equipped with winglet is better than other devices set at the wingtip, winglets are now incorporated into most new commercial and military transport jets. The concept of the winglet is very simple, disconnecting the roll-up vortices from the lower wing surface. A typical civil transport aircraft reveals that the skin friction and lift induced drag together represent more than 80% of the total drag, they constitute of two main sources of drag, approximately one half and one third of t
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Book chapters on the topic "Spiroid winglets"

1

Dhileep, Karthick, S. Arunvinthan, and S. Nadaraja Pillai. "Aerodynamic Characteristics of Semi-spiroid Winglets at Subsonic Speed." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-2718-6_20.

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Conference papers on the topic "Spiroid winglets"

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Kim, Subin. "Experimental Characterization of the Aeroacoustics of a Box-like Spiroid Winglet." In 2024 Regional Student Conferences, Region I - North East. American Institute of Aeronautics and Astronautics, 2024. https://doi.org/10.2514/6.2024-90597.

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