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1 Truesdell, C.A Fluid Dynamics / Str??mungsmechanik I04581 1960 eBook  
2 Truesdell, C.A Fluid Dynamics I / Str??mungsmechanik I I00095 1959 eBook  
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TitleFluid Dynamics / Str??mungsmechanik
Author(s)Truesdell, C.A
PublicationBerlin, Heidelberg, Springer Berlin Heidelberg, 1960.
DescriptionVIII, 816 p : online resource
Abstract NoteSect 2. 317 tinuity surfaces 1. This suggests that a wake pressure Pw be associated with each flow past a bluff body, and that a wake parameter (2. 4) which plays the same role as the cavitation parameter (2. 1), be defined for the flow. This idea has been made the basis of a modified wake theory (ef. Sect. 11) which proves to be in good qu- titative agreement with pressure and drag measurements. It should be emphasized, however, that un?? h like the cavitation number, the wake parameter is a quantity which is not known a priori, and must be empirically determined in each case. (3) Jet flows. The problem of jet efflux from an orifice is one of the oldest in hydrodynamics and the first to be treated by Fig. 3a. the HELMHOLTZ free streamline theory. Of particular importance for engineering applications is the discharge coefficient Cd' which is defined in terms of the discharge Q per unit time, the pressure P, and the cross-sectional area A of the orifice, by the formula, (2. 5) where e is the fluid density. Two methods of measuring Cd have been most fre?? quently adopted. In the first the liquid issues from an orifice in a large vessel under the influence of gravity _,-____________ . , (Fig. 3 a), while in the second it 1 L is forced out of a nozzle or pipe under high pressure (Fig. 3 b)
ISBN,Price9783642459443
Keyword(s)1. EBOOK 2. EBOOK - SPRINGER 3. Engineering Fluid Dynamics 4. FLUID MECHANICS 5. Fluid- and Aerodynamics 6. FLUIDS
Item TypeeBook
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I04581     On Shelf    

2.    
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TitleFluid Dynamics I / Str??mungsmechanik I
Author(s)Truesdell, C.A
PublicationBerlin, Heidelberg, Springer Berlin Heidelberg, 1959.
DescriptionVI, 472 p : online resource
Abstract Note343 Whilst this may be so it is also true that this in itself is not sufficient to deter?? mine it completely. In fact the extent of the dead air region and the behaviour of the shear layer are also of prime importance and in short a unified treatment comprising external flow, boundary layer, shear layer and dead air region becomes necessary to complete the investigation. This would take us outside the scope of the present article and for the substantial progress that has been made towards such a treatment the reader is referred to a paper by HOLDER and GADD 1 and its comprehensive list of references. v. Heat transfer in incompressible boundary layers. 25. Introduction. The term fluid includes gases and liquids. Both gases and liquids are to some extent compressible but in many problems of fluid flow the density changes occurring are small. When they are small enough to be negligible we can regard the flow as incompressible. In Chap. IV we have established the equations for compressible flow of gases and these can of course be used to deter?? mine when density changes in a gas flow are in fact negligible. Broadly speaking this will be so when the temperature changes as determined by the energy equation are small enough
ISBN,Price9783642459146
Keyword(s)1. EBOOK 2. EBOOK - SPRINGER 3. Engineering Fluid Dynamics 4. FLUID MECHANICS 5. Fluid- and Aerodynamics 6. FLUIDS
Item TypeeBook
Multi-Media Links
Please Click here for eBook
Circulation Data
Accession#  Call#StatusIssued ToReturn Due On Physical Location
I00095     On Shelf    

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