Treffer: Wing drag prediction and decomposition
Title:
Wing drag prediction and decomposition
Authors:
Source:
Journal of aircraft. 43(1):82-90
Publisher Information:
Reston, VA: American Institute of Aeronautics and Astronautics, 2006.
Publication Year:
2006
Physical Description:
print, 22 ref
Original Material:
INIST-CNRS
Subject Terms:
Aeronautics astronautics, Aéronautique, astronautique, Mechanical engineering, Génie mécanique, Mechanics acoustics, Mécanique et acoustique, Transportation, Transports, Sciences exactes et technologie, Exact sciences and technology, Physique, Physics, Domaines classiques de la physique (y compris les applications), Fundamental areas of phenomenology (including applications), Mécanique des fluides, Fluid dynamics, Méthodes de calcul en mécanique des fluides, Computational methods in fluid dynamics, Mécanique des fluides appliquée, Applied fluid mechanics, Aérodynamique, Aerodynamics, Aile, Wing, Ala, Aérodynamique, Aerodynamics, Code calcul, Computation code, Código computación, Ecoulement subsonique, Subsonic flow, Ecoulement transsonique, Transonic flow, Ecoulement tridimensionnel, Three dimensional flow, Flujo tridimensional, Fluide visqueux, Viscous fluids, Génération maille, Mesh generation, Mécanique fluide numérique, Computational fluid dynamics, Portance, Lift, Sillage, Wakes, Simulation numérique, Digital simulation, Traînée, Drag
Document Type:
Konferenz
Conference Paper
File Description:
text
Language:
English
Author Affiliations:
University of California, Davis, Davis, California 95616, United States
ISSN:
0021-8669
Rights:
Copyright 2006 INIST-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
CC BY 4.0
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
Notes:
Physics: fluid mechanics
Accession Number:
edscal.17486321
Database:
PASCAL Archive
Weitere Informationen
A wake integration methodology to predict the aerodynamic characteristics of three-dimensional wings in viscous subsonic and transonic flows is presented. Results indicate that wake integration is viable as a method of drag prediction and, compared to surface integration, has the added benefit of being able to provide a decomposition of the total drag into its physical components of profile, induced, and wave drag for a wing in viscous, transonic flow. Future work will involve using wake integration on postprocess flows about more complex configurations for which this study provides a sound basic framework.