Author: T. C Adamson (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
This project was begun in 1979 as a study of three dimensional transonic flows through channels and between compressor blades. In the latter problem, the blades were to be lightly loaded. In 1981, a three year study with the broadened goal of studying flow problems in turbomachines was initiated. Specifically, the work was to include a continuation of that in progress on three-dimensional transonic flows through a lightly loaded compressor blade row, supersonic flow over a compression ramp with a turbulent boundary layer, and consideration of transonic flows over heavily loaded blades in a compressor, starting with a two-dimensional cascade and then going to a three-dimensional rotor if the calculations for the cascade was successful. The work in heavily loaded cascades was to build on the experience gained in the lightly loaded case. The work on the compression ramp has application at blade-shroud interfaces in transonic and supersonic flows. Asymptotic methods of analysis have been employed in all the problems to be described, with numerical methods of solution used as needed in some of the inner regions of the flow fields and to illustrate results for example problems.
Three-Dimensional Flow in Compressors and Channels
Author: T. C Adamson (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
This project was begun in 1979 as a study of three dimensional transonic flows through channels and between compressor blades. In the latter problem, the blades were to be lightly loaded. In 1981, a three year study with the broadened goal of studying flow problems in turbomachines was initiated. Specifically, the work was to include a continuation of that in progress on three-dimensional transonic flows through a lightly loaded compressor blade row, supersonic flow over a compression ramp with a turbulent boundary layer, and consideration of transonic flows over heavily loaded blades in a compressor, starting with a two-dimensional cascade and then going to a three-dimensional rotor if the calculations for the cascade was successful. The work in heavily loaded cascades was to build on the experience gained in the lightly loaded case. The work on the compression ramp has application at blade-shroud interfaces in transonic and supersonic flows. Asymptotic methods of analysis have been employed in all the problems to be described, with numerical methods of solution used as needed in some of the inner regions of the flow fields and to illustrate results for example problems.
Publisher:
ISBN:
Category :
Languages : en
Pages : 23
Book Description
This project was begun in 1979 as a study of three dimensional transonic flows through channels and between compressor blades. In the latter problem, the blades were to be lightly loaded. In 1981, a three year study with the broadened goal of studying flow problems in turbomachines was initiated. Specifically, the work was to include a continuation of that in progress on three-dimensional transonic flows through a lightly loaded compressor blade row, supersonic flow over a compression ramp with a turbulent boundary layer, and consideration of transonic flows over heavily loaded blades in a compressor, starting with a two-dimensional cascade and then going to a three-dimensional rotor if the calculations for the cascade was successful. The work in heavily loaded cascades was to build on the experience gained in the lightly loaded case. The work on the compression ramp has application at blade-shroud interfaces in transonic and supersonic flows. Asymptotic methods of analysis have been employed in all the problems to be described, with numerical methods of solution used as needed in some of the inner regions of the flow fields and to illustrate results for example problems.
Three-dimensional Flow in Core Compressors
Author: James Michael Macgregor Place
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Three Dimensional Flow in Compressor Cascades
Author: Massachusetts Institute of Technology. Gas Turbine Laboratory
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 110
Book Description
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 110
Book Description
Three-dimensional Flow Visualization in a Centrifugal Compressor
Author: William Lee Trevillion
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 90
Book Description
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 90
Book Description
ASME 68-GT-2
Unsteady Three-dimensional Flow in a Compressor Cascade with Inlet Flow Distortions
Author: Saeed Farokhi
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 226
Book Description
Publisher:
ISBN:
Category : Cascades (Fluid dynamics)
Languages : en
Pages : 226
Book Description
Measurement and Calculation of the Three-dimensional Flow in Axial Compressor Stators, with and Without End-bends
Author: C. J. Robinson (Writer on compressors)
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Compressors
Languages : en
Pages : 0
Book Description
Aerodynamic Design of Axial Flow Compressors
Author: Robert O. Bullock
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 552
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 552
Book Description
Aerodynamic Design of Axial-flow Compressors
Author: Lewis Research Center
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 542
Book Description
Publisher:
ISBN:
Category : Axial flow compressors
Languages : en
Pages : 542
Book Description