Family
4-digit
Camber
2.0%
Position
40%
Thick.
12%
Regime
Subsonic
Solver
LBM
Shock
Mixed
Avg. |u|
0.04 lattice u.
Max. |u|
0.10 lattice u.
Pressure Drop
0.00e+0 lattice Δp
Aerodynamic Coefficients
0.00 CL
CD 0.00 · L/D 0.0
Fx 0.0e+0 · Fy 0.0e+0
Kutta-Joukowski
0.00 CLΓ
Γ 0.00 · L′ 0.00
CM
0.00
CP min
0.00
CP max
0.00
Mach
—
Solver
LBM
Dwave
0.0e+0
Flow
subsonic
Shock
normal
Subsonic values use D2Q9 LBM pressure. Transonic, supersonic, and hypersonic airfoil values use the compressible shock-field solver with normal or oblique shock structure.
|u| / Uinlet