Cartesian Mesh Linearized Euler Equations Solver for Aeroacoustic Problems around Full Aircraft

Table 5

Mesh information for calculations of noise propagation around the fuselage-wing-nacelle configurations.

	Minimum cell size	Number of cubes	Number of cells in one cube	Total number of cells	PPW
DLR-F6	0.0025D	3,474	50 × 50 × 50	434,250,000	9.0
OWN	0.0025D	3,425	50 × 50 × 50	428,125,000	9.0