NDLI: Tads: a cfd-based turbomachinery and analysis design system with gui. volume 2: user's manual

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Tads: a cfd-based turbomachinery and analysis design system with gui. volume 2: user's manual

Content Provider	NASA Technical Reports Server (NTRS)
Author	Topp, D. A. Myers, R. A. Delaney, R. A.
Copyright Year	1995
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.
File Size	2854363
Page Count	86
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19960010174
Archival Resource Key	ark:/13960/t8wb03q7j
Language	English
Publisher Date	1995-12-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Turbomachine Blades Cascade Flow Internal Flow Three Dimensional Flow Computational Fluid Dynamics Graphical User Interface Airfoils Applications Programs Computers Computer Aided Design User Manuals Computer Programs Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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