Librería: ISD LLC, Bristol, CT, Estados Unidos de America
Original o primera edición
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Añadir al carritopaperback. Condición: New. 1st.
Librería: GreatBookPrices, Columbia, MD, Estados Unidos de America
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Añadir al carritoCondición: As New. Unread book in perfect condition.
Librería: GreatBookPrices, Columbia, MD, Estados Unidos de America
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Idioma: Inglés
Publicado por Logos Verlag Berlin GmbH, Berlin, 2012
ISBN 10: 3832532285 ISBN 13: 9783832532284
Librería: Grand Eagle Retail, Bensenville, IL, Estados Unidos de America
EUR 71,34
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Añadir al carritoPaperback. Condición: new. Paperback. Aero engine bearing chambers are complex machine elements inside the engines, supporting up to three concentric shafts on bearings. For safety reasons, the aero engines always employ rolling-element type bearings and therefore require a sufficient oil supply for lubrication in order to guarantee a reliable operation. As a consequence, a complex two-phase flow consisting of oil and sealing air governs the bearing chambers. A highly dynamic oil film, flowing along the chamber walls, plays a vital role to fulfill the tasks of cooling, lubricating and cleaning the bearing chambers. The design and optimization process of the bearing chambers requires a detailed understanding in order to accurately simulate the film behaviour inside the bearing chambers. Based on the earlier experimental investigations, it is known that near the scavenge off-take a relatively thick film exists. The numerical model to simulate these films must therefore take into account the elliptical behaviour of such films. Among the different models, the Volume Of Fluid (VOF) Model offers the best compromise between accuracy and efforts.However, preliminary attempts to model a fully developed and turbulent test case from literature revealed an unphysical pressure drop and velocity profile in the gas phase above the film flow. An inadequate turbulence modelling near the gas-liquid interface was identified as the problem source. The 2-Equation turbulence models were extended to achieve a substantial improvement. Shipping may be from multiple locations in the US or from the UK, depending on stock availability.
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Añadir al carritoCondición: New. 2012. Paperback. . . . . .
Librería: Russell Books, Victoria, BC, Canada
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Añadir al carritoPaperback. Condición: Brand New. 142 pages. 9.75x7.00x0.50 inches. In Stock.
Librería: GreatBookPricesUK, Woodford Green, Reino Unido
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Añadir al carritoCondición: New. 2012. Paperback. . . . . . Books ship from the US and Ireland.
Idioma: Inglés
Publicado por Logos Verlag Berlin GmbH, Berlin, 2012
ISBN 10: 3832532285 ISBN 13: 9783832532284
Librería: AussieBookSeller, Truganina, VIC, Australia
EUR 116,15
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Añadir al carritoPaperback. Condición: new. Paperback. Aero engine bearing chambers are complex machine elements inside the engines, supporting up to three concentric shafts on bearings. For safety reasons, the aero engines always employ rolling-element type bearings and therefore require a sufficient oil supply for lubrication in order to guarantee a reliable operation. As a consequence, a complex two-phase flow consisting of oil and sealing air governs the bearing chambers. A highly dynamic oil film, flowing along the chamber walls, plays a vital role to fulfill the tasks of cooling, lubricating and cleaning the bearing chambers. The design and optimization process of the bearing chambers requires a detailed understanding in order to accurately simulate the film behaviour inside the bearing chambers. Based on the earlier experimental investigations, it is known that near the scavenge off-take a relatively thick film exists. The numerical model to simulate these films must therefore take into account the elliptical behaviour of such films. Among the different models, the Volume Of Fluid (VOF) Model offers the best compromise between accuracy and efforts.However, preliminary attempts to model a fully developed and turbulent test case from literature revealed an unphysical pressure drop and velocity profile in the gas phase above the film flow. An inadequate turbulence modelling near the gas-liquid interface was identified as the problem source. The 2-Equation turbulence models were extended to achieve a substantial improvement. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability.