International Journal of Aerospace Engineering / 2018 / Article / Tab 2

Research Article

Propulsive Efficiency of Ridge/Inlet Configuration

Table 2

Main grids in CFD simulations.

GridCell number (million) (Pa)

M1 (method 1)0.91128,679.9
M2 (method 1)2.47118,892.1
N1 (method 1)4.26117,486.3
N2 (method 1)5.26117,579.1
N35.81117,581.8
N4 (results are presented in the current paper, method 1)6.38117,589.6
N5 (different internal mesh structure)6.48117,585.3