Sentence examples for drag coefficient can be from inspiring English sources

The Strouhal number and the drag coefficient can be considered 0.12 and (C_{{{text{D}}0}}) = 0.2, respectively, for a wide range of Reynolds numbers.

In case of an oscillating body, the drag coefficient can be approximated to 2, so that the value of (gamma) is obtained as 1.32.

In doing so, the Courant number must be reduced to adapt the temporal scale in such a way that an accurate average of the lift and drag coefficient can be obtained.

Moreover, an increase in shear parameter decreases the peak response amplitude but broadens the lock-in range over which large oscillation amplitudes occur; the virtual local drag coefficient can be significantly higher than the nominal value.

We illustrate the proposed approach by carrying out lift and/or drag optimization for the NACA 0012 airfoil containing a rectangular fuel tank: By identifying polynomial response surfaces using a large batch of 1800 design candidates, we conclude that the lift coefficient can be optimized by a linear model, whereas the drag coefficient can be optimized by using a quadratic model.

The results of this research, which can be applied to any new car design, show configurations in which the overall drag coefficient can be decreased by 2%, the aerodynamic cooling drag coefficient by more than 50% and the lift coefficient by 5%.

When the propellers are positioned after sucking peak, the longer the area which the propellers work on, the more the profile drag coefficients can be reduced.

Our previous practice in Multi-Scale Computational Fluid Dynamics (MSCFD), which is characterized by coupling of TFM and EMMS drag coefficient, can then be viewed as a simplified realization of EFM.

As orbital decay can be measured with relative accuracy, and its mechanism broken down into its constituent sources, the value of drag-related coefficients can be inferred by fitting modelled orbit predictions to observed data wherein the coefficient of interest is the adjusted parameter.

The results show that the drag coefficient and the resultant of the lift and side forces coefficients can be described by an empirical function of the incidence angle.

After optimization, the transition delay can be up to 17% and the aerodynamic drag coefficient can decrease by 12.1%.