Unified Theoretical Foundations of Lift and Drag in Viscous and Compressible External Flows / by Luo-Qin Liu
By: Liu, Luo-Qin
Contributor(s): SpringerLink (Online service)
Material type:
E-bookSeries: (Springer Theses, Recognizing Outstanding Ph.D. Research,, 2190-5053); (Engineering (Springer-11647)).Publisher: Singapore : Springer International Publishing, 2018Description: 1 recurso en línea (XIX, 154 páginas) : 19 ilustraciones, 18 ilustraciones a color.ISBN: 9789811062230.Subject: Aerodinámica
Abstract: This thesis analyzes aerodynamic forces in viscous and compressible external flows. It is unique, as the force theories discussed apply to fully viscous and compressible Navier-Stokes external flows, allowing them to be readily combined with computational fluid dynamics to form a profound basis of modern aerodynamics. This thesis makes three fundamental contributions to theoretical aerodynamics, presenting: (1) a universal far-field zonal structure that determines how disturbance flow quantities decay dynamically to the state of rest at infinity; (2) a universal and exact total-force formula for steady flow and its far-field asymptotics; and (3) a general near-field theory for the detailed diagnosis of all physical constituents of aerodynamic force and moment.
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|
LIBRO-E NO PRÉSTAMO
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Madrid Digital Acceso Electrónico (UEM) | Ciencias e Ingeniería | TL570 2018 EB (Browse shelf(Opens below)) | Acceso electrónico | eBook.15112750 |
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This thesis analyzes aerodynamic forces in viscous and compressible external flows. It is unique, as the force theories discussed apply to fully viscous and compressible Navier-Stokes external flows, allowing them to be readily combined with computational fluid dynamics to form a profound basis of modern aerodynamics. This thesis makes three fundamental contributions to theoretical aerodynamics, presenting: (1) a universal far-field zonal structure that determines how disturbance flow quantities decay dynamically to the state of rest at infinity; (2) a universal and exact total-force formula for steady flow and its far-field asymptotics; and (3) a general near-field theory for the detailed diagnosis of all physical constituents of aerodynamic force and moment.
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