Download 3D-Computation of Incompressible Internal Flows: Proceedings by Gabriel Sottas, Inge L. Ryhming PDF

By Gabriel Sottas, Inge L. Ryhming

The goal of the 1989 GAMM Workshop on 3D-Computation of Incompressible inner Flows was once the simulation of a pragmatic incompressible stream box in a massive commercial program. In view of the problems considering formulating this sort of try out case, requiring the provision of an experimental information base, severe care needed to be taken within the number of the correct one. Professor I. L. Ryhming's inspiration, that the circulate via a Francis turbine configuration or elements thereof will be possible as a try out case, as a result of the numerical demanding situations in addition to the chance to provide an experimental facts base through the use of the experimental amenities of the Hydraulic Machines and Fluid Mechanics Institute (IMHEF) on the Swiss Federal Institute of expertise in Lausanne (EPFL), was once approved through the GAMM Committee in April 1987. a systematic committee, shaped less than the chairmanship of Professor I. L. Ryhming, met a couple of times to choose the Francis turbine configuration, the try out case requisites, and so forth. , wherein the layout enter got here from the water turbine specialists. This committee made up our minds to limit the reports to the 3 following standard purposes for the easiest working element of the turbine: • simulation of the 3D circulation in a Francis runner in rotation • simulation of the 3D movement within the distributor (stay and consultant vane earrings) of this turbine • simulation of the 3D movement in an elbow draft tube The simultaneous computation of 2 or 3 of those geometries was once encouraged.

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Additional resources for 3D-Computation of Incompressible Internal Flows: Proceedings of the GAMM Workshop held at EPFL, 13–15 September 1989, Lausanne, Switzerland

Sample text

40 .... 40 40 20 60 I I 80 100 120 1 I + Cp Stayrlng Inlet 165' .... SO o 40 20 60 I I 80 100 ... 60 + Cp .... 30 -0040 . "Cu +Cz ..... J.. - A ........ / .... Curvilinear abscissa [mm] - o 20 40 60 I I 80 100 Fig. 072, respectively, and the guide-vane opening angle IX is 25". Stay ring inlet Data corresponding to the flow survey at the stayring inlet is given in Figure 16. Static and total pressure coefficients Cp and Cpt and coefficients corresponding to the three flow velocity components are provided versus the traversing axis coordinates.

E. Npa = 21). 24 The arclength s associated with a point (R, Z) on the axis is the length of the portion of axis joining the band point of the axis to the point (R, Z). The associated nonnalized arclength s* is then simply the arclength s divided by Rref. 47 [mm). The reason of requiring averaged values for the pressure coefficient and for the velocity components is the same as for Requirement 2. Requirement 4 c;, c~, c:, c;', a and fJ along the leading and the trailing edges of the blade versus the normalized arclength along the edge.

J................... /+...................... 32 ~1! ~..... j . lI.. j ..................... , ");':'" ! - '::'"c,+•... ; .....! •.. 8 1 Distance along traverse from band b Fig.

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