TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 1: Method and Results PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 1: Method and Results PDF full book. Access full book title TADS: A CFD-based Turbomachinery and Analysis Design System with GUI. Volume 1: Method and Results by . Download full books in PDF and EPUB format.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
Get Book Here
Book Description
Author: M. J. Koiro
Publisher:
ISBN:
Category :
Languages : en
Pages : 144
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 164
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 90
Get Book Here
Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721078264
Category :
Languages : en
Pages : 160
Get Book Here
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 the Final Report describing the theoretical basis and analytical results from the TADS system developed under 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) or a 3-D solver with slip condition on the end walls (B2BADPAC) 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 multistage compressor, a multistage turbine, two highly loaded fans, and several single stage compressor and turbine example cases. Koiro, M. J. and Myers, R. A. and Delaney, R. A. Glenn Research Center NAS3-27394; RTOP 538-03-11
Author: Terry Wright
Publisher: CRC Press
ISBN: 9780849320156
Category : Technology & Engineering
Languages : en
Pages : 380
Get Book Here
Book Description
Fluid Machinery: Performance, Analysis, and Design provides a comprehensive introduction to the fluid mechanics of turbomachinery. By focusing on the preliminary design and selection of equipment to meet a set of performance specifications-including size, noise, and cost limitations-the author promotes a basic but thorough understanding of the subject. His pragmatic approach exposes students to a realistic array of conflicting requirements and real-world industrial applications, while providing a solid background for more advanced study. Coveriage of both gas and hydraulic turbines and emphasis on industrial issues and equipment makes this book ideal for mechanical engineering students. Fluid Machinery uses extensive illustration, examples, and exercises to prepare students to confront industrial applications with confidence.
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722794712
Category :
Languages : en
Pages : 86
Get Book Here
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 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
Get Book Here
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 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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100
Get Book Here
Book Description
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721011773
Category :
Languages : en
Pages : 96
Get Book Here
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
