TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 2: User's Manual PDF Download
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Author:
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Category :
Languages : en
Pages : 90
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722794712
Category :
Languages : en
Pages : 86
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The primary objective of this study was the development of a computational fluid dynamics (CFD) based turbomachinery airfoil analysis and design system, controlled by a graphical user interface (GUI). The computer codes resulting from this effort are referred to as the Turbomachinery Analysis and Design System (TADS). This document is intended to serve as a user's manual for the computer programs which comprise the TADS system. TADS couples a throughflow solver (ADPAC) with a quasi-3D blade-to-blade solver (RVCQ3D) in an interactive package. Throughflow analysis capability was developed in ADPAC through the addition of blade force and blockage terms to the governing equations. A GUI was developed to simplify user input and automate the many tasks required to perform turbomachinery analysis and design. The coupling of various programs was done in a way that alternative solvers or grid generators could be easily incorporated into the TADS framework. Myers, R. A. and Topp, D. A. and Delaney, R. A. Unspecified Center...
Author: National Aeronautics and Space Adm Nasa
Publisher:
ISBN: 9781730948121
Category :
Languages : en
Pages : 88
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The primary objective of this study was the development of a computational fluid dynamics (CFD) based turbomachinery airfoil analysis and design system, controlled by a graphical user interface (GUI). The computer codes resulting from this effort are referred to as the Turbomachinery Analysis and Design System (TADS). This document is intended to serve as a user's manual for the computer programs which comprise the TADS system. TADS couples a throughflow solver (ADPAC) with a quasi-3D blade-to-blade solver (RVCQ3D) in an interactive package. Throughflow analysis capability was developed in ADPAC through the addition of blade force and blockage terms to the governing equations. A GUI was developed to simplify user input and automate the many tasks required to perform turbomachinery analysis and design. The coupling of various programs was done in a way that alternative solvers or grid generators could be easily incorporated into the TADS framework. Myers, R. A. and Topp, D. A. and Delaney, R. A. Unspecified Center...
Author: M. J. Koiro
Publisher:
ISBN:
Category :
Languages : en
Pages : 85
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Author:
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ISBN:
Category :
Languages : en
Pages : 100
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721011773
Category :
Languages : en
Pages : 96
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Book Description
The primary objective of this study was the development of a Computational Fluid Dynamics (CFD) based turbomachinery airfoil analysis and design system, controlled by a Graphical User Interface (GUI). The computer codes resulting from this effort are referred to as TADS (Turbomachinery Analysis and Design System). This document is intended to serve as a User's Manual for the computer programs which comprise the TADS system, developed under Task 18 of NASA Contract NAS3-27350, ADPAC System Coupling to Blade Analysis & Design System GUI and Task 10 of NASA Contract NAS3-27394, ADPAC System Coupling to Blade Analysis & Design System GUI, Phase II-Loss, Design and, Multi-stage Analysis. TADS couples a throughflow solver (ADPAC) with a quasi-3D blade-to-blade solver (RVCQ3D) in an interactive package. Throughflow analysis and design capability was developed in ADPAC through the addition of blade force and blockage terms to the governing equations. A GUI was developed to simplify user input and automate the many tasks required to perform turbomachinery analysis and design. The coupling of the various programs was done in such a way that alternative solvers or grid generators could be easily incorporated into the TADS framework. Results of aerodynamic calculations using the TADS system are presented for a highly loaded fan, a compressor stator, a low speed turbine blade and a transonic turbine vane.Koiro, M. J. and Myers, R. A. and Delaney, R. A.Glenn Research CenterTURBOMACHINERY; USER MANUALS (COMPUTER PROGRAMS); COMPUTATIONAL FLUID DYNAMICS; GRAPHICAL USER INTERFACE; COMPUTER PROGRAMS; DESIGN ANALYSIS; SYSTEMS ANALYSIS; STATORS; VANES; TURBINE BLADES
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Category :
Languages : en
Pages : 126
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Category :
Languages : en
Pages :
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Author:
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ISBN:
Category :
Languages : en
Pages : 164
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Author: M. J. Koiro
Publisher:
ISBN:
Category :
Languages : en
Pages : 144
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