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Transonic Blade-to-Blade Flows in Axial Turbomachinery

Transonic Blade-to-Blade Flows in Axial Turbomachinery PDF Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Transonic Blade-to-Blade Flows in Axial Turbomachinery

Transonic Blade-to-Blade Flows in Axial Turbomachinery PDF Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


Transonic Flows in Axial Turbomachinery

Transonic Flows in Axial Turbomachinery PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 300

Book Description


Transonic Flow Problems in Turbomachinery

Transonic Flow Problems in Turbomachinery PDF Author: Thomas Charles Adamson
Publisher:
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 724

Book Description


Tronsonic Flows in Axial Turbomachinery

Tronsonic Flows in Axial Turbomachinery PDF Author:
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ISBN:
Category :
Languages : en
Pages :

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

Book Description


Transonic Flow Around Compressor Rotor Blade Elements. Volume I. Analysis

Transonic Flow Around Compressor Rotor Blade Elements. Volume I. Analysis PDF Author: John W. Kurzrock
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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

Improved Method for Calculating Transonic Velocities on Blade-to-blade Stream Surfaces of a Turbomachine PDF Author: Jerry R. Wood
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32

Book Description


Aeronautical Engineering

Aeronautical Engineering PDF Author:
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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

Fluid Mechanics, Acoustics, and Design of Turbomachinery PDF Author: B. Lakshminarayana
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ISBN:
Category : Fluid mechanics
Languages : en
Pages : 468

Book Description


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 540

Book Description