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Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings by D. Vijayaraghavan
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1NASA Technical Reports Server (NTRS) 19910006991: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings
By NASA Technical Reports Server (NTRS)
An analogy between the mathematical modeling of transonic potential flow and the flow in a cavitating bearing is described. Based on the similarities, characteristics of the cavitated region and jump conditions across the film reformation and rupture fronts are developed using the method of weak solutions. The mathematical analogy is extended by utilizing a few computational concepts of transonic flow to numerically model the cavitating bearing. Methods of shock fitting and shock capturing are discussed. Various procedures used in transonic flow computations are adapted to bearing cavitation applications, for example, type differencing, grid transformation, an approximate factorization technique, and Newton's iteration method. These concepts have proved to be successful and have vastly improved the efficiency of numerical modeling of cavitated bearings.
“NASA Technical Reports Server (NTRS) 19910006991: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19910006991: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
“NASA Technical Reports Server (NTRS) 19910006991: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings” Subjects and Themes:
- Subjects: ➤ NASA Technical Reports Server (NTRS) - ANALOGIES - BEARINGS - CAVITATION FLOW - COMPUTATIONAL FLUID DYNAMICS - FLUID FILMS - POTENTIAL FLOW - TRANSONIC FLOW - ANALYSIS (MATHEMATICS) - FACTORIZATION - FINITE DIFFERENCE THEORY - FITTING - ITERATION - MATHEMATICAL MODELS - Vijayaraghavan, D. - Keith, T. G., Jr. - Brewe, D. E.
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19910006991
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 20.72 Mbs, the file-s for this book were downloaded 60 times, the file-s went public at Sun Sep 25 2016.
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2DTIC ADA231726: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings
By Defense Technical Information Center
In this paper, an analogy between the mathematical modeling of transonic potential flow and the flow in a cavitating bearing is described. Based on the similarities, characteristics of the cavitated region and jump conditions across the film reformation and rupture fronts are developed using the method of weak solutions. The mathematical analogy is extended by utilizing a few computational concepts of transonic flow to numerically model the cavitating bearing. Methods of shock fitting and shock capturing are discussed. Various procedures used in transonic flow computations are adapted to bearing cavitation applications, for example, type differencing, grid transformation, an approximate factorization technique, and Newton's iteration method. These concepts have proved to be successful and have vastly improved the efficiency of numerical modeling of cavitated bearings.
“DTIC ADA231726: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings” Metadata:
- Title: ➤ DTIC ADA231726: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA231726: Extension Of Transonic Flow Computational Concepts In The Analysis Of Cavitated Bearings” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Vijayaraghavan, D - NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CENTER - *MATHEMATICAL MODELS - GRIDS - SOLUTIONS(GENERAL) - SHOCK - MATHEMATICS - CAVITATION - TRANSFORMATIONS - POTENTIAL FLOW - TRANSONIC FLOW - ANALOGIES - FITTINGS - COMPUTATIONS - LOW STRENGTH
Edition Identifiers:
- Internet Archive ID: DTIC_ADA231726
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 13.28 Mbs, the file-s for this book were downloaded 56 times, the file-s went public at Wed Feb 28 2018.
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