Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-3510
Full metadata record
DC FieldValueLanguage
dc.contributor.authorDa Ronch, Andrea-
dc.contributor.authorVentura, Antonino-
dc.contributor.authorRighi, Marcello-
dc.contributor.authorFranciolini, Matteo-
dc.contributor.authorBerci, Marco-
dc.contributor.authorKharlamov, Daniel-
dc.date.accessioned2018-02-20T16:05:22Z-
dc.date.available2018-02-20T16:05:22Z-
dc.date.issued2018-
dc.identifier.issn1000-9361de_CH
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/2882-
dc.description.abstractAnalytical indicial aerodynamic functions are calculated for several trapezoidal wings in subsonic flow, with a Mach number 0.3≤ Ma≤ 0.7. The formulation herein proposed extends well-known aerodynamic theories, which are limited to thin aerofoils in incompressible flow, to generic trapezoidal wing planforms. Firstly, a thorough study is executed to assess the accuracy and limitation of analytical predictions, using unsteady results from two state-of-the-art computational fluid dynamics solvers as cross-validated benchmarks. Indicial functions are calculated for a step change in the angle of attack and for a sharp-edge gust, each for four wing configurations and three Mach numbers. Then, analytical and computational indicial responses are used to predict dynamic derivatives and the maximum lift coefficient following an encounter with a one-minus-cosine gust. It is found that the analytical results are in excellent agreement with the computational results for all test cases. In particular, the deviation of the analytical results from the computational results is within the scatter or uncertainty in the data arising from using two computational fluid dynamics solvers. This indicates the usefulness of the developed analytical theories.de_CH
dc.language.isoende_CH
dc.publisherElsevierde_CH
dc.relation.ispartofChinese Journal of Aeronauticsde_CH
dc.rightshttp://creativecommons.org/licenses/by-nc-nd/4.0/de_CH
dc.subjectIndicial aerodynamicsde_CH
dc.subjectAnalytical approachde_CH
dc.subjectCFDde_CH
dc.subjectTrapezoidal wingde_CH
dc.subjectCompressible flowde_CH
dc.subjectGust responsede_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleExtension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flowde_CH
dc.typeBeitrag in wissenschaftlicher Zeitschriftde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitInstitut für Mechanische Systeme (IMES)de_CH
dc.identifier.doi10.21256/zhaw-3510-
dc.identifier.doi10.1016/j.cja.2018.02.008de_CH
zhaw.funding.euNode_CH
zhaw.issue4de_CH
zhaw.originated.zhawYesde_CH
zhaw.pages.end631de_CH
zhaw.pages.start617de_CH
zhaw.publication.statusacceptedVersionde_CH
zhaw.volume31de_CH
zhaw.publication.reviewPeer review (Publikation)de_CH
zhaw.webfeedTechnikkommunikationde_CH
Appears in collections:Publikationen School of Engineering

Files in This Item:
File Description SizeFormat 
1-s2.0-S1000936118300621-main.pdf1.48 MBAdobe PDFThumbnail
View/Open
Show simple item record
Da Ronch, A., Ventura, A., Righi, M., Franciolini, M., Berci, M., & Kharlamov, D. (2018). Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow. Chinese Journal of Aeronautics, 31(4), 617–631. https://doi.org/10.21256/zhaw-3510
Da Ronch, A. et al. (2018) ‘Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow’, Chinese Journal of Aeronautics, 31(4), pp. 617–631. Available at: https://doi.org/10.21256/zhaw-3510.
A. Da Ronch, A. Ventura, M. Righi, M. Franciolini, M. Berci, and D. Kharlamov, “Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow,” Chinese Journal of Aeronautics, vol. 31, no. 4, pp. 617–631, 2018, doi: 10.21256/zhaw-3510.
DA RONCH, Andrea, Antonino VENTURA, Marcello RIGHI, Matteo FRANCIOLINI, Marco BERCI und Daniel KHARLAMOV, 2018. Extension of analytical indicial aerodynamics to generic trapezoidal wings in subsonic flow. Chinese Journal of Aeronautics. 2018. Bd. 31, Nr. 4, S. 617–631. DOI 10.21256/zhaw-3510
Da Ronch, Andrea, Antonino Ventura, Marcello Righi, Matteo Franciolini, Marco Berci, and Daniel Kharlamov. 2018. “Extension of Analytical Indicial Aerodynamics to Generic Trapezoidal Wings in Subsonic Flow.” Chinese Journal of Aeronautics 31 (4): 617–31. https://doi.org/10.21256/zhaw-3510.
Da Ronch, Andrea, et al. “Extension of Analytical Indicial Aerodynamics to Generic Trapezoidal Wings in Subsonic Flow.” Chinese Journal of Aeronautics, vol. 31, no. 4, 2018, pp. 617–31, https://doi.org/10.21256/zhaw-3510.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.