Space shuttle

Results of simulation of airflow hydrodynamics around the space shuttle.
The shuttle geometry from NASA 3D open resources library.

Grid statistics:
Total number of computational nodes = 21 018 446
Number of fluid (1) nodes = 20 441 199
Number of bounce back (61) nodes = 471 777
Number of velocity (20) nodes = 52 735
Number of velocity0 (40) nodes = 0
Number of pressure (30) nodes = 52 735
Number of periodic (4) and (5) nodes = 0
Ratio of non-fluid nodes to total number of computational nodes [%] = 2.74638

Solution parameters:
Re = 2800
U_Ch_LB = 0.14
Dt_phys [s] = 0.599999
L_ch_LB [Lu] = 200
Nu_LB = 0.00999999

Solver: Microflow 3D R0.1
Data visualisation software: ParaView v5.6