drag coefficient


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Related to drag coefficient: Drag force
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Synonyms for drag coefficient

the ratio of the drag on a body moving through air to the product of the velocity and the surface area of the body

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References in periodicals archive ?
CFD - Computational fluid dynamics RANS - Reynolds-averaged Navier-Stokes LES - Large eddy simulation SST - Shear stress transport DNS - Direct numerical simulation [C.sub.1] - Lift coefficient [C.sub.d] - Drag coefficient [C.sub.p] - Pressure coefficient C - Main element fixed chord length [y.sup.+] - Non-dimensional wall distance [G.sub.f1] - Flap 1 gap [G.sub.f2] - Flap 2 gap [O.sub.f1] - Flap 1 overlap [O.sub.f2] - Flap 2 overlap [[delta].sub.f1] - Flap 1 deflection [[delta].sub.f2] - Flap 2 deflection VI.
In our discussion on how to determine BC, we must have a discussion about what drag coefficient (Cd) is.
(i) A drag coefficient correlation that takes into account the effect of the bubble shape through the Eotvos number and the effect of the contaminants present in the system used.
where [CL.sub.0] is the lift coefficient of the rigid wing and [CD.sub.0] is the drag coefficient. This model will also be called only once.
Moreover, the total drag coefficient and Nusselt number are computed in this range of conditions: Ri = 0-4, Re = 10-40, at Pr = 1.
This technology allows cyclists to test and refine their drag coefficient in everyday riding conditions, without having to use expensive and time-consuming wind tunnel testing.
(3) [rho] is the fluid density, A the cross-sectional area of the particle, [c.sub.d] the drag coefficient and v the velocity of the fluid.
Based on the testing data, the relationship of the drag coefficient and the Reynolds number were derived for the chain.
The drag coefficient is closely related to particle geometry.
Table 1: Characteristic design Parameters Chord 0.4167 ft Lift Curve Slope 4.712 /rad Min Lift Coefficient -1.1 Max Lift Coefficient 1.1 Drag Coefficient Gain 0.9 Drag Coefficient Offset 0.9 Duct Moment Coefficient 0.8 Table 2: Mesh details Mesh type Hybrid mesh (tetra/prism) Global element size 0.04 Prism mesh 0.004 Prism mesh layers around duct 6 Total mesh elements 5,48,446 Mesh nodes 95,317 Table 3: Result Analysis L/D ratio for duct 3.686 L/uD ratio for ducted propeller 3.862
This study indicates the independency of the results from the mesh density and as the mesh density increases from 5 to 10 million elements, the drag coefficient ranges from 0.250 to 0.266 for Standard k - [epsilon] and 0.20 to 0.23 for Realizable k - [epsilon].
The aerodynamic characteristic parameters of the ice-coated conductor include drag coefficient, lift coefficient, and torsional coefficient.
The independence of the mesh is verified by assessing the root mean square (RMS) of the lift coefficient and the mean drag coefficient for different mesh densities.
All these data will be used to estimate parameters such as the drag coefficient ([C.sub.adj]).
where [F.sub.d,w] and [F.sub.l,w] denote the drag force and lift force, [C.sub.d,w] and [C.sub.l,w] denote the drag coefficient and lift coefficient, aw denotes the angle of attack, [[rho].sub.air] denotes the air density, U denotes the wind velocity, and [D.sub.r,w] denotes the maximum height of windward side of cross section and it is approximately equal to the diameter of cross section.