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• Main Page
  3 KB (468 words) - 12:59, 13 March 2023
• QNET-CFD-Main
  #REDIRECT [[Category:QNET-CFD Main]]
  36 bytes (4 words) - 19:48, 29 August 2009

Page text matches

• QNET-CFD-Main
  #REDIRECT [[Category:QNET-CFD Main]]
  36 bytes (4 words) - 19:48, 29 August 2009
• Description AC3-02
  ...France in Chatou, France. A high Reynolds number flow is maintained in the main pipe while very small incoming mass flow rates are imposed in the auxiliary ...l power in the dead leg is directly affected by the Reynolds number in the main pipe and by geometric details of the junction, whereas the influence of the
  5 KB (768 words) - 16:00, 11 February 2017
• Evaluation AC3-10
  The CFD results have been used to calculate the pressure drops between the main branch (leg 1) and each of the two secondary branches (legs 2 and 3) for ea Figure 8 – Coarse mesh at main branch inlet
  3 KB (370 words) - 16:12, 11 February 2017
• Evaluation AC1-08
  ...ction. In addition, the CFD simulation predicts a greater spreading of the main element wake at this location than indicated by the experiment. ...d that the CFD code tends to under predict the mixing between the slat and main element wakes.
  3 KB (528 words) - 15:08, 11 February 2017
• NavTree
  **[[QNET-CFD-Main|Main Category]]
  3 KB (317 words) - 10:56, 17 October 2019
• Best Practice Advice AC3-02
  ...l power in the dead leg is directly affected by the Reynolds number in the main pipe and by geometric details of the junction, whereas the influence of the A high Reynolds number developed turbulent flow is maintained in the main pipe while very small incoming mass flow rates are imposed in the auxiliary
  6 KB (983 words) - 16:02, 11 February 2017
• Best Practice Advice AC1-09
  is characterized by the main vortex developing above the wing. The vortex is ...er downstream. This is necessary to capture the initial development of the main vortex and the turbulence within the vortex.
  4 KB (620 words) - 15:20, 11 February 2017
• ECARP README
  for you, named "extract_data", that you will also find in the main directory.
  2 KB (342 words) - 11:28, 11 April 2010
• Description AC2-01
  ...both the bluff-body jet flames discussed here consist, generally, of three main zones: stabilisation, extinction and reignition zones. ...diameters are 3.6 mm for the fuel nozzle and 50mm for the bluff-body. The main fuel jet composition is 50% CH4 and 50% H2 for a bulk Jet velocity of 118,
  7 KB (1,076 words) - 15:26, 11 February 2017
• Description AC1-08
  ...element (deflection angle <math>25^0</math>), and a Fowler flap aft of the main element (deflection angle <math>20^0</math>). See Figure 1. Measurements we ...ure of the L1T2 profile. It consists of a main element, slat and flap. The main element comprises a BAC 3-11/RES/30/21 section and the overall chord of the
  7 KB (1,061 words) - 15:07, 11 February 2017
• Evaluation AC1-09
  the main vortex (and some also a smaller peak due to secondary separation), whereas the experiment shows a plateau. In the computations, the main vortex
  11 KB (1,855 words) - 15:19, 11 February 2017
• UFR 3-15 Description
  ...e there is also a second bubble at the top wall. In the turbulent case the main recirculation zone is smaller and a secondary bubble appears inside this re The main features to be compared in this test case are the general pattern of the st
  6 KB (979 words) - 13:28, 12 February 2017
• DynamicPageList Demo
  **[[KB-Wiki-Main|Main Category]]
  4 KB (534 words) - 10:51, 17 January 2021
• UFR 4-05 Best Practice Advice
  ...by the interaction of the pressure gradient linked to the curvature of the main flow with the non-uniform flow. The flow, moving slower in the boundary lay ...of 29 simulations performed on the DLR turbine stator and coming from two main studies.
  3 KB (519 words) - 14:10, 12 February 2017
• UFR 1-05 Evaluation
  * With the large eddy simulations, two main discrepancies have been found in the comparison of results with experiments ...and Kavsaoglu was based on a Reynolds number of 51400 with respect to the main stream velocity and the jet pipe diameter. This Reynolds number may be equi
  3 KB (528 words) - 19:07, 11 February 2017
• CFD Simulations AC1-08
  A no-slip and adiabatic boundary condition was applied on the slat, main-element and flap solid surfaces. The simulation was performed in “free-ai ...set the turbulent viscosity to zero ahead of the transition points on the main element as well as turning off the source terms in the turbulent kinetic en
  9 KB (1,353 words) - 16:48, 14 February 2017
• UFR 2-01 Description
  ...the unsteady flow phenomena, which appears behind the turbine blades. The main characteristic of the proposed UFR is the vortex shedding, which is generat According to Sieverding et al. (2002) the main characteristics of such flows are:
  7 KB (996 words) - 19:29, 11 February 2017
• UFR 3-35 Description
  ...V1) (Baker 1980). The saddle point S1 devides the fluid entrained into the main vortex from the one contributing to the near-wall jet.
  5 KB (797 words) - 15:50, 4 November 2020
• Evaluation AC7-04
  ...n capturing main flow features, such as the small separation region in the main branch at peak systole and the recirculation in the aneurysm and the back f ...ts associated recirculation at the junction between the collateral and the main descending duct (cf. Fig. 13) could explained this overestimation due to ve
  8 KB (1,269 words) - 18:14, 16 February 2022
• CFD Simulations AC3-02
  ...pipe lengths to minimize the size of the numerical model. The inlet of the main pipe has been placed relatively near from the junction to reduce the size o ...pipe), Dirichlet conditions are used for all transported variables. In the main pipe, the incoming flow is supposed to be fully developed. Hence, the mean
  10 KB (1,338 words) - 16:01, 11 February 2017