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=== Underlying Flow Regime 3-32 === The flow under investigation is an oblique shock reflection on a flat

=Mixing ventilation flow in an enclosure driven by a transitional wall jet= === Underlying Flow Regime 4-20 ===

...codes, the fact that it contains no assumptions related to the combustion regime, and the possibility of directly employing a chemical reaction mechanism of ...sed volumes caused by the different shapes of the reaction zones in the FC regime. This was in corroboration with earlier findings, also pointed in the concl

=== Underlying Flow Regime 3-34 === Major geometric and flow parameters of the TC are presented in [[UFR_3-34_Test_Case#figure2|Fig.&nbs

Underlying Flow Regime 1-07 # <span id="3">Xin, Y., Baroclinic effects on fire flow field, in ''Proc. 4th Joint Meeting of the U.S. Section of the Combustion I

Briefly describe the key fluid physics/flow regimes which exert an influence on the DOAPs. Ideally thi ...number for air in the trachea is 4920, which is well within the turbulent regime.

Underlying Flow Regime 1-06 The density and other flow properties (molecular viscosity,

=== Underlying Flow Regime 2-15 === The main flow bulk parameters obtained in the different wind tunnel and numerical studies

= Flow over curved backward-facing step = === Underlying Flow Regime 3-31 ===

= 2D flow over backward facing step = Underlying Flow Regime 3-15 <font size="-2" color="#888888"> © copyright ERCOFTAC 2

=== Underlying Flow Regime 1-07 === having a core region of higher momentum flow surrounded by shear layers

=== Underlying Flow Regime 2-15 === ...sly mentioned, BARC addresses the high Reynolds number, external, unsteady flow over a stationary,

...iveness. It is used in a wide range of design applications, whenever fluid flow, heat transfer, combustion or many other complicated processes are signific ...f the experimental and theoretical works devoted to the instability of the flow types important for aero-engine combustors.

=Fluid-structure interaction in turbulent flow past cylinder/plate configuration I (First swiveling mode)= === Underlying Flow Regime 2-13 ===

=Fluid-structure interaction in turbulent flow past cylinder/plate configuration I (First swiveling mode)= === Underlying Flow Regime 2-13 ===

Underlying Flow Regime 3-01 <font size="-2" color="#888888"> © copyright ERCOFTAC 2

= Flow in a 3D diffuser = === Underlying Flow Regime 4-16 ===

Underlying Flow Regime 1-07 * The flow through the orifice is laminar.

Underlying Flow Regime 1-06 There was no evidence of laminar flow behaviour at a position two inlet

Underlying Flow Regime 1-01 <font size="-2" color="#888888">               © copyright ER In summary, the underlying-flow-regime considered here has been that of the under-expanded jet, of which there are