Author: Theodore Katsanis
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 93
Book Description
A FORTRAN 4 computer program has been developed that obtains a subsonic or shock-free transonic flow solution on the hub-shroud mid-channel flow surface of a turbomachine. The blade row may be fixed or rotating, and may be twisted and leaned. Flow may be axial or mixed, up to 45 deg from axial. Upstream and downstream flow variables may vary from hub to shroud, and provision is made to correct for loss of stagnation pressure. The results include velocities, streamlines, and flow angles on the flow surface; and approximate blade surface velocities. Subsonic solutions are obtained by a finite-difference stream-function solution. Transonic solutions are obtained by a velocity-gradient method, using information from a finite-difference stream-function solution at a reduced mass flow.
FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Mid-channel Flow Surface of an Axial- Or Mixed-flow Turbomachine. 1: User's Manual
Author: Theodore Katsanis
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 93
Book Description
A FORTRAN 4 computer program has been developed that obtains a subsonic or shock-free transonic flow solution on the hub-shroud mid-channel flow surface of a turbomachine. The blade row may be fixed or rotating, and may be twisted and leaned. Flow may be axial or mixed, up to 45 deg from axial. Upstream and downstream flow variables may vary from hub to shroud, and provision is made to correct for loss of stagnation pressure. The results include velocities, streamlines, and flow angles on the flow surface; and approximate blade surface velocities. Subsonic solutions are obtained by a finite-difference stream-function solution. Transonic solutions are obtained by a velocity-gradient method, using information from a finite-difference stream-function solution at a reduced mass flow.
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 93
Book Description
A FORTRAN 4 computer program has been developed that obtains a subsonic or shock-free transonic flow solution on the hub-shroud mid-channel flow surface of a turbomachine. The blade row may be fixed or rotating, and may be twisted and leaned. Flow may be axial or mixed, up to 45 deg from axial. Upstream and downstream flow variables may vary from hub to shroud, and provision is made to correct for loss of stagnation pressure. The results include velocities, streamlines, and flow angles on the flow surface; and approximate blade surface velocities. Subsonic solutions are obtained by a finite-difference stream-function solution. Transonic solutions are obtained by a velocity-gradient method, using information from a finite-difference stream-function solution at a reduced mass flow.
Revised FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Midchannel Stream Surface of an Axial-, Radial-, Or Mixed-flow Turbomachine Or Annular Duct: User's manual
Author: Theodore Katsanis
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 116
Book Description
FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Mid-channel Flow Surface of an Axial- Or Mixed-flow Turbomachine
Author: Theodore Katsanis
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 220
Book Description
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 220
Book Description
FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Mid-channel Flow Surface of an Axial- Or Mixed-flow Turbomachine
Author: Theodore Katsanis
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 209
Book Description
A FORTRAN-IV computer program, MERIDL, has been developed that obtains a subsonic or shock-free transonic flow solution on the hub-shroud mid-channel flow surface of a turbomachine. The blade row may be fixed or rotating and may be twisted and leaned. Flow may be axial or mixed, up to 45 deg from axial. Upstream and downstream flow variables can vary from hub to shroud, and provision is made to correct for loss of stagnation pressure. The results include velocities, streamlines, and flow angles on the flow surface and approximate blade surface velocities. Subsonic solutions are obtained by a finite-difference stream-function solution. Transonic solutions are obtained by a velocity-gradient method, using information from a finite-difference stream-function solution at a reduced mass flow.
Publisher:
ISBN:
Category : Turbomachines
Languages : en
Pages : 209
Book Description
A FORTRAN-IV computer program, MERIDL, has been developed that obtains a subsonic or shock-free transonic flow solution on the hub-shroud mid-channel flow surface of a turbomachine. The blade row may be fixed or rotating and may be twisted and leaned. Flow may be axial or mixed, up to 45 deg from axial. Upstream and downstream flow variables can vary from hub to shroud, and provision is made to correct for loss of stagnation pressure. The results include velocities, streamlines, and flow angles on the flow surface and approximate blade surface velocities. Subsonic solutions are obtained by a finite-difference stream-function solution. Transonic solutions are obtained by a velocity-gradient method, using information from a finite-difference stream-function solution at a reduced mass flow.
Revised FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Midchannel Stream Surface of an Axial-, Radial-, Or Mixed-flow Turbomachine Or Annular Duct: Programmer's manual
Author: Theodore Katsanis
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 236
Book Description
Publisher:
ISBN:
Category : FORTRAN (Computer program language)
Languages : en
Pages : 236
Book Description
Revised FORTRAN Program for Calculating Velocities and Streamlines on the Hub-shroud Midchannel Stream Surface of an Axial-, Radial-, Or Mixed-flow Turbomachine Or Annular Duct
Author: Theodore Katsanis
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Revised Fortran Program for Calculating Velocities and Streamlines on the Hub-shroud Midchannel Stream Surface of an Axial-, Radial-, Or Mixed-flow Turbomachine Or Annular Duct. II - Programmer's Manual
Author: Theodore Katsanis
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 492
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 28
Book Description
Fundamental Heat Transfer Research for Gas Turbine Engines
Author:
Publisher:
ISBN:
Category : Gas-turbine industry
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Gas-turbine industry
Languages : en
Pages : 76
Book Description