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    دورية أكاديمية
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    رسالة جامعية

    المؤلفون: Suárez Valdés, Óscar Daniel

    المساهمون: López Mejía, Omar Dario, González Mancera, Andrés Leónardo, Jaramillo Ibarra, Julián Ernesto, Facultad de Ingeniería::Grupo de Mecánica Computacional

    وصف الملف: 116 páginas; application/pdf

    العلاقة: A. W. Schäfer and I. A. Waitz, “Air transportation and the environment,” Transp. policy, vol. 34, pp. 1–4, 2014, doi:10.1016/j.tranpol.2014.02.012; B. Khandelwal, A. Karakurt, P. R. Sekaran, V. Sethi, and R. Singh, “Hydrogen powered aircraft : The future of air transport,” Prog. Aerosp. Sci., vol. 60, pp. 45–59, 2013, doi:10.1016/j.paerosci.2012.12.002; X. Li, M. de Groot, and T. Bäck, “Using forecasting to evaluate the impact of COVID-19 on passenger air transport demand,” Decis. Sci., 2021, doi:10.1111/deci.12549; International Civil Aviation Organization, “Air traffic recovery Is fast approaching pre-pandemic levels”, 2022. [En línea]. Accedido el 22 de noviembre de 2022. Disponible: https://www.icao.int/Newsroom/Pages/ES/Air-traffic-recovery-is-fastapproaching-prepandemic-levels.aspxTest.; T. D’Alfonso, C. Jiang, and V. Bracaglia, “Air transport and high-speed rail competition: Environmental implications and mitigation strategies,” Transp. Res. Part A. Policy Pract., vol. 92, pp. 261–276, 2016, doi:10.1016/j.tra.2016.06.009; J. E. Guerrero, M. Sanguineti, and K. Wittkowski, “Variable cant angle winglets for improvement of aircraft flight performance,” Mecc., vol. 55, no. 10, pp. 1917–1947, 2020, doi:10.1007/s11012-020-01230-1; M. Giuni, “Formation and early development of wingtip vortices,” Ph.D. Dissertation, Dept. of Aerosp. Eng., University of Glasgow, 2013. [En línea]. Disponible: https://theses.gla.ac.uk/3871Test/; J. P. Eguea, P. D. Bravo-Mosquera, and F. M. Catalano, “Camber morphing winglet influence on aircraft drag breakdown and tip vortex structure,” Aerosp. Sci. Technol., vol. 119, p. 107148, 2021, doi:10.1016/j.ast.2021.107148; S. Kapsalis, P. Panagiotou, and K. Yakinthos, “CFD-aided optimization of a tactical Blended-Wing-Body UAV platform using the Taguchi method,” Aerosp. Sci. Technol., vol. 108, p. 106395, 2021, doi:10.1016/j.ast.2020.106395; "Model Description %7C NASA Common Research Model". NASA Common Research Model, providing data worldwide. [En línea]. Disponible: https://commonresearchmodel.larc.nasa.gov/home-2/high-speed-crm/experimental-approach/model-descriptionTest/; “DPW-6,” NASA, Accedido el 18 de mayo de 2023. [En línea]. Disponible: https://aiaa-dpw.larc.nasa.gov/Workshop6/workshop6.htmlTest.; Compute mesh spacing for a given y+ for viscous flow in CFD, Cadence, Accedido el 19 de mayo de 2023. [En línea]. Disponible: https://www.cadence.com/en_US/home/tools/system-analysis/computational-fluid-dynamics/y-plus.htmlTest.; Menter, F. R., “Two-equation eddy-viscosity turbulence models for engineering applications,” AIAA Journal, Vol. 32, No. 8, 1994, pp. 1598–1605. https://doi.org/10.2514/3.12149Test, URL https://doi.org/10.2514/3.12149Test.; “Computational results” NASA, Accedido el 18 de mayo de 2023. [En línea]. Disponible:https://commonresearchmodel.larc.nasa.gov/computational-resultsTest.; University of Oxford, Drag-Prediction Workshop, Accedido el 18 de mayo de 2023. [En línea]. Disponible: https://aiaa-dpw.larc.nasa.gov/Workshop6/presentations/2_01_Oxford-presentation-FINAL.pdfTest; L. Gipson, “National Transonic Facility Overview, NASA, Accedido el 18 de mayo de 2023. [En línea]. Disponible: https://www.nasa.gov/aetc/transonic/ntfTest.; Experimental results, NASA common research model, Accedido el 19 de mayo de 2023. [En línea]. Disponible: https://commonresearchmodel.larc.nasa.gov/experimental-dataTest; H. Gutiérrez Pulido and R. de la Vara Salazar, Análisis y diseño de experimentos, 2a ed. México: McGraw-Hill, 2008. van Dam, C. P. (2003). "Aircraft design and the importance of drag prediction". CFD-Based Aircraft Drag Prediction and Reduction. pp. 1–37; van Dam, C. P. (2003). "Aircraft design and the importance of drag prediction". CFD-Based Aircraft Drag Prediction and Reduction. pp. 1–37.; Runze LI, Kaiwen DENG, Yufei ZHANG, Haixin CHEN, “Pressure distribution guided supercritical wing optimization”, Chinese Journal of Aeronautics, vol. 31, pp. 1842-1854, 2018, doi:10.1016/j.cja.2018.06.021; “Practical CFD Modeling: Turbulence”. DMS Marine Consultant. Accedido el 10 de diciembre de 2023. [En línea]. Disponible: https://www.dmsonline.us/practical-cfd-modeling-turbulenceTest/; “Box-Behnken designs”. Information Technology Laboratory %7C NIST. Accedido el 15 de octubre de 2023. [En línea]. Disponible: https://www.itl.nist.gov/div898/handbook/pri/section3/pri3362.htmTest; Gracia-Salcedo CM, Brabbs TA, McBride BJ. Experimental verification of the thermodynamic properties of Jet-A fuel. NASA technical memorandum 101475; 1988.; “ExxonMobil Jet Fuel”. ExxonMobil. Accedido el 10 de diciembre de 2023. [En línea]. Disponible: https://www.exxonmobil.com/en-bd/commercial-fuel/pds/gl-xx-jetfuel-seriesTest; “Airport compatibility, 787 Airplane Characteristics for Airport Planning”. The Boeing Company Official Website. Accedido el 20 de enero de 2024. [En línea]. Disponible: https://www.boeing.com/resources/boeingdotcom/commercial/airports/acaps/787.pdfTest; T. W. Anderson and D. A. Darling, (1954), A test of goodness of fit, J. Amer. Stat. Assn., 49 765–769.; Ralph B. DAgostino (1986). "Tests for the Normal Distribution". In DAgostino, R.B.; Stephens, M.A. (eds.). Goodness-of-Fit Techniques. New York: Marcel Dekker. ISBN 0-8247-7487-6.; https://hdl.handle.net/1992/73403Test; instname:Universidad de los Andes; reponame:Repositorio Institucional Séneca; repourl:https://repositorio.uniandes.edu.coTest/

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    دورية أكاديمية

    المصدر: Molecules

    العلاقة: ANID Fondecyt regular [1191528, 1210107]; ANID CONICYT PIA/APOYO CCTE [AFB170007]; ANID International Collaboration [REDES 190181, R17A10003, ACE210016]; ANID fondecyt iniciacion [11190325]; info:eu-repo/grantAgreement/MESTD/Integrated and Interdisciplinary Research (IIR or III)/43009/RS//; https://vinar.vin.bg.ac.rs/handle/123456789/10100Test; 000736506000001; 2-s2.0-85121538935; http://vinar.vin.bg.ac.rs/bitstream/id/25971/molecules-26-07477-v2.pdfTest