A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability

The work reported in the present paper was performed to honor the centennial of the flight by Alberto Santos Dumont with his 14-Bis aircraft. The paper describes results for a computational fluid dynamics (CFD) analysis of the 14-Bis aircraft aerodynamics and flight stability. The 14-Bis aircraft ge...

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Main Authors: Leonardo Ostan Bitencourt, Gregori Pogorzelski, Ramon Morais de Freitas, João Luiz F. Azevedo
Format: Article
Language:English
Published: Departamento de Ciência e Tecnologia Aeroespacial 2011-05-01
Series:Journal of Aerospace Technology and Management
Subjects:
CFD
Online Access:http://www.jatm.com.br/papers/vol3_n2/JATMv3n2_p137-146_A_CFD-based_analysis_of_the_14-Bis_aircraft_aerodynamics_and_stability.pdf
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spelling doaj-b8b724b8b5f6425cb2453ad90eee131c2020-11-24T22:15:14ZengDepartamento de Ciência e Tecnologia AeroespacialJournal of Aerospace Technology and Management1984-96482175-91462011-05-0132137146A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability Leonardo Ostan BitencourtGregori PogorzelskiRamon Morais de FreitasJoão Luiz F. AzevedoThe work reported in the present paper was performed to honor the centennial of the flight by Alberto Santos Dumont with his 14-Bis aircraft. The paper describes results for a computational fluid dynamics (CFD) analysis of the 14-Bis aircraft aerodynamics and flight stability. The 14-Bis aircraft geometry was generated from historical sources and observations. CFD computations were performed using well-established commercial codes for calculation of the historical flight conditions. Simulations considered a Reynolds-averaged Navier-Stokes formulation, in which turbulence closure was achieved by using Menter's model. The flight conditions investigated were primarily concerned with historical observations regarding flight speeds and the need for a more powerful engine, as well as flight stability characteristics of the 14-Bis airplane, which are unknown up to the present day. The results led to qualitative agreement with historical reports, although quite interesting conclusions could be drawn with regard to the actual aerodynamic flight speeds and the aircraft stability parameters.http://www.jatm.com.br/papers/vol3_n2/JATMv3n2_p137-146_A_CFD-based_analysis_of_the_14-Bis_aircraft_aerodynamics_and_stability.pdfAerodynamicsCFDCentennial of flightSantos Dumont14-Bis aircraft
collection DOAJ
language English
format Article
sources DOAJ
author Leonardo Ostan Bitencourt
Gregori Pogorzelski
Ramon Morais de Freitas
João Luiz F. Azevedo
spellingShingle Leonardo Ostan Bitencourt
Gregori Pogorzelski
Ramon Morais de Freitas
João Luiz F. Azevedo
A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
Journal of Aerospace Technology and Management
Aerodynamics
CFD
Centennial of flight
Santos Dumont
14-Bis aircraft
author_facet Leonardo Ostan Bitencourt
Gregori Pogorzelski
Ramon Morais de Freitas
João Luiz F. Azevedo
author_sort Leonardo Ostan Bitencourt
title A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
title_short A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
title_full A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
title_fullStr A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
title_full_unstemmed A CFD-based analysis of the 14-Bis aircraft aerodynamics and stability
title_sort cfd-based analysis of the 14-bis aircraft aerodynamics and stability
publisher Departamento de Ciência e Tecnologia Aeroespacial
series Journal of Aerospace Technology and Management
issn 1984-9648
2175-9146
publishDate 2011-05-01
description The work reported in the present paper was performed to honor the centennial of the flight by Alberto Santos Dumont with his 14-Bis aircraft. The paper describes results for a computational fluid dynamics (CFD) analysis of the 14-Bis aircraft aerodynamics and flight stability. The 14-Bis aircraft geometry was generated from historical sources and observations. CFD computations were performed using well-established commercial codes for calculation of the historical flight conditions. Simulations considered a Reynolds-averaged Navier-Stokes formulation, in which turbulence closure was achieved by using Menter's model. The flight conditions investigated were primarily concerned with historical observations regarding flight speeds and the need for a more powerful engine, as well as flight stability characteristics of the 14-Bis airplane, which are unknown up to the present day. The results led to qualitative agreement with historical reports, although quite interesting conclusions could be drawn with regard to the actual aerodynamic flight speeds and the aircraft stability parameters.
topic Aerodynamics
CFD
Centennial of flight
Santos Dumont
14-Bis aircraft
url http://www.jatm.com.br/papers/vol3_n2/JATMv3n2_p137-146_A_CFD-based_analysis_of_the_14-Bis_aircraft_aerodynamics_and_stability.pdf
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