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  • === Underlying Flow Regime 3-36 === ...). Geometric variations of the test case were designed to achieve attached flow, incipient, moderate and strong separation. For the incipient configuration
    6 KB (958 words) - 15:51, 17 February 2023
  • Underlying Flow Regime 1-06 <li>The flow can be treated as axisymmetric.</li>
    5 KB (713 words) - 19:15, 11 February 2017
  • Underlying Flow Regime 3-11 <font size="-2" color="#888888">               © copyright ER ...documented here, flow and heat transfer in a pipe expansion, relates to a flow geometry which is often encountered in industrial applications. Although th
    7 KB (1,042 words) - 13:09, 12 February 2017
  • = Flow around airfoils (and blades) A-airfoil (Ma=0.15,<br />Re/m=2x10<sup>6</sup> Underlying Flow Regime 2-05 <font size="-2" color="#888888"> © copyright ERCOFTAC 2
    4 KB (522 words) - 19:43, 11 February 2017
  • ===Underlying Flow Regime 3-32=== ...>'''Smits A.J., Dussauge J.P.''' 2006 Turbulent shear layers in supersonic flow, Second edition, Springer Verlag, New York, NY, USA.</div>
    4 KB (522 words) - 13:46, 12 February 2017
  • === Underlying Flow Regime 3-34 === The UFR in question is characterized by several complex flow phenomena. They include APG-induced separation of the turbulent boundary la
    7 KB (1,002 words) - 11:08, 15 March 2018
  • Underlying Flow Regime 3-01 <font size="-2" color="#888888"> © copyright ERCOFTAC 2 ...cs of a high&ndash;lift system [1, 2], and the numerical simulation of the flow over a high-lift system is considered to be a very challenging CFD problem,
    6 KB (1,003 words) - 12:25, 12 February 2017
  • The key fluid physics and flow regimes which influence the design or assessment parameters (the jet spread * the ratio of the background (upward) flow velocity to the jet (downward) flow velocity
    10 KB (1,618 words) - 15:49, 11 February 2017
  • Underlying Flow Regime 3-18 <font size="-2" color="#888888">               © copyright ER ...drag which in turn affect vehicle handling and fuel consumption. Internal flow separation in expanding ducts create nonuniformities degrade the life of co
    6 KB (853 words) - 13:32, 12 February 2017
  • = Turbulent Flow Past Two-Body Configurations = === Underlying Flow Regime 2-12 ===
    6 KB (900 words) - 12:06, 12 February 2017
  • Underlying Flow Regime 1-01 <font size="-2" color="#888888">               © copyright ER ...listic applications, is usually a combination of many different underlying flow processes. One aspect of QNET-CFD is to identify all these important compon
    15 KB (2,278 words) - 19:00, 11 February 2017
  • ===Underlying Flow Regime 4-19=== there are interesting flow features present in the flow and their capturing is a considerable challenge for turbulence models.
    11 KB (1,723 words) - 14:47, 12 February 2017
  • =Flow and heat transfer in a pin-fin array= ===Underlying Flow Regime 4-18===
    6 KB (902 words) - 14:43, 12 February 2017
  • = Flow over curved backward-facing step = === Underlying Flow Regime 3-31 ===
    7 KB (1,064 words) - 13:41, 12 February 2017
  • = Flow around oscillating airfoil = Underlying Flow Regime 2-03 <font size="-2" color="#888888"> © copyright ERCOFTAC 2
    8 KB (1,146 words) - 19:35, 11 February 2017
  • ...ressure field. The correct swirl profile is also implicitly coupled to the flow reversal which creates the two streams that transport the classified produc 1.3. The constrained free vortex flow in a cyclone means that turbulent fluctuations are restrained in the tangen
    13 KB (2,014 words) - 16:06, 11 February 2017
  • ===Underlying Flow Regime 2-15=== ...'''Arslan, T., Pettersen B., Andersson H.I.''', 2011. Calculations of the flow around rectangular shaped floating structures, In: Proceedings of the thirt
    17 KB (2,315 words) - 12:18, 12 February 2017
  • =Mixing ventilation flow in an enclosure driven by a transitional wall jet= === Underlying Flow Regime 4-20 ===
    7 KB (1,084 words) - 11:33, 2 March 2018
  • =Flow over curved backward-facing step= ===Underlying Flow Regime 3-31===
    7 KB (1,008 words) - 13:43, 12 February 2017
  • Underlying Flow Regime 4-09 <font size="-2" color="#888888"> © copyright ERCOFTAC 2 AEA 1995 ''Computational Fluid Dynamics Services CFX 4.1 Flow Solver''. User Guide (Harwell: AEA)
    5 KB (686 words) - 14:21, 12 February 2017
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