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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Heat and mass transfer 25 (1990), S. 111-116 
    ISSN: 1432-1181
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Description / Table of Contents: Zusammenfassung In dieser Untersuchung wurde eine Prozedur zur numerischen Lösung von nichtviskoser Rotationsströmung über eine dreidimensionale Flügelkonfiguration entwickelt. Diese Prozedur löst die dreidimensionalen Eulergleichungen in einem angepaßten Koordinatensystem und in einer strikten Erhaltungsform. Das Delta-ADI-Faktorisierungsverfahren wird entwickelt und angewandt um die resultierenden algebraischen Gleichungen zu lösen. Mittels der Newtonschen Linearisierungstechnik wurde schnelle Konvergenz erreicht. Die vorliegende Prozedur wurde in FORTRAN programmiert. Der Programmname ist „WING3D“. Eine Reihe von Testrechnungen wurden durchgeführt, um die Gültigkeit und die Exaktheit der Prozedur und des Programmes zu testen. Schließlich wurde das Programm für transsonische Strömung (M ∞ = 0.84) über einen rechtwinkeligen Flügel mit einem Anströmwinkel von 3.06° und einem Seitenverhältnis von 14 gestartet. Die Ergebnisse werden in Isobaren und Machlinien von verschiedenen Stellen des Flügels dargestellt, diskutiert und analysiert. Die Eigenschaften des Aufpralls auf die oberen und unteren Oberflächen werden dargestellt.
    Notes: Abstract A solution procedure is developed for the numerical solution of inviscid rotational flow past three-dimensional wing configuration. This procedure solves the three-dimensional Euler equations in a body-fitted coordinate system and strong conservation form. The delta ADI approximate finite-difference factorization technique is developed and used to solve the resulting set of algebraic equations. Fast convergence was attained by using the Newton linearization technique. The present procedure is coded into a FORTRAN program called “WING3D”. A number of test cases were conducted to check the validity and the accuracy of the procedure and the code. Finally the code was run for transonic flow (M ∞ = 0.84) over a rectangular wing at angle of attack of 3.06° and aspect ratio of 14. The results are plotted in pressure curves and mach contours at different sections along the wing. The solutions are discussed and analysed. The shock properties on the upper and lower surfaces are demonstrated.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Heat and mass transfer 23 (1988), S. 55-60 
    ISSN: 1432-1181
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Description / Table of Contents: Zusammenfassung In der vorliegenden Arbeit wird das numerische Modell über die Wärmespeicherung in einem Wirbelbett der oben genannten Autoren [5] verbessert und in eine dimensionslose Form umgearbeitet. Das verbesserte Modell basiert auf neuere Experimente bei unterschiedlichen Lufteintrittstemperaturen. Zwischen den numerischen und den experimentellen Ergebnissen wird eine sehr gute Übereinstimmung erzielt. Das neue Modell wird für die Durchführung einer ausführlichen Parameterstudie verwendet. Damit soll der Einfluß der dimensionslosen Parameter (α2, α3 und α4) auf die Leistung des Wirbelbettes bestimmt, sowie die Bedingungen für eine günstige Arbeitsweise des Bettes aufgezeigt, und die Leistung des Wirbelbettes mit der eines Festbettes zu verglichen werden. Die numerischen Ergebnisse werden anhand des zeitlichen Verlaufes der Bett-Temperatur $$\bar \theta _b $$ und des Bett-Wirkungsgrades(η) dargestellt. Der Leistungsverlauf wird für verschiedene Werte der einzelnen Parameter (α2,α3 und α4) angegeben. Die Studie zeigt, daß das Wirbelbett sich für α2 〈 10, α3 〉 30 und α3 〈 10 am günstigsten verhält. Ferner kam man zu dem Ergebnis, daß das Festbett im allgemeinen bei gleicher Bettgröße und gleicher Wärmezufuhr ein besseres Leistungsverhalten bietet.
    Notes: Abstract In the present work, the numerical model developed earlier by the same authors [5] is refined and recast in non-dimensional form. The refined model is calibrated with recent experiments at different bed air-inlet temperatures. Excellent agreement between the numerical results and experiments is obtained. The refined model is then used to conduct an extensive parametric study. The objectives of the parametric study are: (i) to determine the effect of the non-dimensional parameters (α2, α3 and α4) on the bed performance; (ii) to indicate the conditions required for favourable bed operation, and (iii) to compare the fluidized-bed performance with a small-particle packed bed performance. The numerical results are presented as time-histories of average bed temperature ( $$\bar \theta _b $$ ) and bed efficiency(η). The performance histories are given for different value of each parameter (α2, α3, and α4). The study shows that the fluidized bed behaves favourably for α2 〈 10, α3〉 30 and α4 〈 10. Moreover, it was concluded that the small particle packed bed, in general, offers better performance behaviour over a fluidized bed having the same bed size and heat input.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Springer
    Heat and mass transfer 23 (1988), S. 187-194 
    ISSN: 1432-1181
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Description / Table of Contents: Zusammenfassung Es wird die Wirbelschichtleistung untersucht, wenn diese an einen parabolischen Solarkonzentrator gekoppelt ist. Die Methode benutzt das eindimensionale Wirbelschichtmodell in Verbindung mit einem Solarkonzentrator-Empfänger-Modell. Eine analytische Untersuchung der verschiedenen Auslegungsparameter, wie z. B. die Konzentrationsrate, die Blende des Konzentrators und die Größe der Wirbelschicht wird durchgeführt. Die Ergebnisse werden schließlich benutzt um eine Beziehung zwischen Leistung und Auslegungsparametern zu erhalten, welche dann benutzt werden kann, um die Konstruktion eines Wirbelschicht-Konzentrator-Speichersystems zu optimieren.
    Notes: Abstract The fluidized bed performance is predicted when it is coupled to a solar parabolic concentrator. The prediction method uses the one dimensional fluidized bed model in connection to a solar concentrator-receiver model. An analytical study of the different design parameters such as the concentration ratio, concentrator aperture area and the size of the fluidized bed is presented. The results are then used to obtain a correlation between some performance and design parameters, which can be used to optimize the design of the fluidized bed-concentrator storage system.
    Type of Medium: Electronic Resource
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  • 4
    Electronic Resource
    Electronic Resource
    Springer
    Flow, turbulence and combustion 55 (1995), S. 119-139 
    ISSN: 1573-1987
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract A boundary element-wake numerical approach is developed and used to determine all drag components of a three dimensional body in a wind tunnel flow. The approach decomposes the total drag into three components; the profile drag, the cross flow drag (induced drag), and the tunnel-wall effect component, each with its own physical significance. Additionally, the cross flow drag component is divided into two components, the vortex component and the source (dilatation) component. In the present approach, the transverse kinematics relations are expressed as integral representations of the axial vorticity and the transverse dilatation (source strength). This advantage permits the vortex and the source drag computations to be performed only in the vortical area of the transverse wake and hence avoids excessive computations. Also, the procedures distinguish the contribution of the transverse dilatation to the cross flow drag. The validity of the present procedure is examined by comparing the present results against the experimental data of reference [1] for a car and wing models. The comparison shows that the present computed total drag, for the wing and the car models, agrees very well with the experimental data, provided that the wake data are measured at survey planes moderately distant from the body.
    Type of Medium: Electronic Resource
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  • 5
    Electronic Resource
    Electronic Resource
    Chichester : Wiley-Blackwell
    International Journal for Numerical Methods in Fluids 28 (1998), S. 477-499 
    ISSN: 0271-2091
    Keywords: natural convection ; tilted cavity ; partial cooling ; storage tanks ; Engineering ; Numerical Methods and Modeling
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Two-dimensional numerical simulations of laminar natural convection in a partially cooled, differentially heated inclined cavities are performed. One of the cavity walls is entirely heated to a uniformly high temperature (heat source) while the opposite wall is partially cooled to a lower temperature (heat sink). The remaining walls are adiabatic. The tilt angle of the cavity is varied from 0° (heated from left) to -90° (heated from top). The fast false implicit transient scheme (FITS) algorithm, developed earlier by the same authors, is modified to solve the derived variables vorticity-streamfunction formulation. The effects of aspect ratio (AR), sink-source ratio and tilt angle on the average Nusselt number are examined through a parametric study; solutions are obtained for two Grashof numbers, 105 and 107. Flow patterns and isotherms are used to investigate the heat transfer and fluid flow mechanisms inside the cavity. © 1998 John Wiley & Sons, Ltd.
    Additional Material: 9 Ill.
    Type of Medium: Electronic Resource
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