Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Transonic Blade-to-Blade Flows in Axial Turbomachinery
Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Transonic Flows in Axial Turbomachinery
Transonic Flow Problems in Turbomachinery
Author: Thomas Charles Adamson
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 724
Book Description
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 724
Book Description
Tronsonic Flows in Axial Turbomachinery
Scientific and Technical Aerospace Reports
Transonic Flow Around Compressor Rotor Blade Elements. Volume I. Analysis
Author: John W. Kurzrock
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
A numerical technique has been developed to obtain a solution for steady, transonic blade element flow in an axial compressor rotor of a turbomachine. Radius variation and stream surface convergence are included. The mixed-out exit conditions include shock wave losses and viscous mixing losses. The time-dependent Navier-Stokes equations in conservation law form are cast in a relative coordinate system suitable for describing rotor blade element flow. A discretized method of characteristics is used to determine the boundary conditions along the blade surface and exit plane. Steady, supersonic, uniform flow conditions are specified at upstream infinity, and periodicity is enforced on the remaining free boundaries. The hyperbolic/parabolic system of equations describing the mixed flow problem are approximated by the explicit MacCormack finite-difference scheme. The time-dependent numerical solution rapidly converges to a steady-state result. Comparisons are made with experimental data for two-dimensional cascade flows and rotor blade element flow. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description
A numerical technique has been developed to obtain a solution for steady, transonic blade element flow in an axial compressor rotor of a turbomachine. Radius variation and stream surface convergence are included. The mixed-out exit conditions include shock wave losses and viscous mixing losses. The time-dependent Navier-Stokes equations in conservation law form are cast in a relative coordinate system suitable for describing rotor blade element flow. A discretized method of characteristics is used to determine the boundary conditions along the blade surface and exit plane. Steady, supersonic, uniform flow conditions are specified at upstream infinity, and periodicity is enforced on the remaining free boundaries. The hyperbolic/parabolic system of equations describing the mixed flow problem are approximated by the explicit MacCormack finite-difference scheme. The time-dependent numerical solution rapidly converges to a steady-state result. Comparisons are made with experimental data for two-dimensional cascade flows and rotor blade element flow. (Author).
Improved Method for Calculating Transonic Velocities on Blade-to-blade Stream Surfaces of a Turbomachine
Author: Jerry R. Wood
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Fluid Mechanics, Acoustics, and Design of Turbomachinery
Author: B. Lakshminarayana
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 468
Book Description
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 468
Book Description