TY - JOUR
T1 - Moving sphere simulations using the chimera grid approach
AU - Schauerhamer, Daniel Guy
AU - Hauser, Thomas
PY - 2009
Y1 - 2009
N2 - Steady and unsteady cases with moving spheres were computed using the Chimera Grid Approach and OVERFLOW, a compressible Reynolds Averaged Navier-Stokes flow solver. The cases modeled situations encountered with agricultural seeding machines. Central differencing with scalar TLNS3D dissipation for spatial terms and implicit Euler time advancement were used. First, a sphere moving with a constant velocity away from a suction orifice was computed and the resulting forces were compared with experimental values. Second, one sphere was dropped and allowed to move under the influence of aerodynamic and gravitational forces with six degrees of freedom. Third, two spheres were dropped similar to the second case this time taking collisions between the two spheres into account. The force data compared with experimental data averaged an 8% error for 3.5 kPa suction out of the orifice, and 13% for 1.75 kPa suction out of the orifice, and 4% error for a 3.5 kPa suction case with second order dual time stepping. For the sphere drop cases, the desired behavior was known by experimentalists, and was achieved with minimal error. Testing on 8 to 96 processors with a 6.616 million grid point mesh demonstrated nearly linear speedup. Through the investigation, it was shown that the Chimera Grid Approach used with OVERFLOW is a valid choice for moving mesh applications.
AB - Steady and unsteady cases with moving spheres were computed using the Chimera Grid Approach and OVERFLOW, a compressible Reynolds Averaged Navier-Stokes flow solver. The cases modeled situations encountered with agricultural seeding machines. Central differencing with scalar TLNS3D dissipation for spatial terms and implicit Euler time advancement were used. First, a sphere moving with a constant velocity away from a suction orifice was computed and the resulting forces were compared with experimental values. Second, one sphere was dropped and allowed to move under the influence of aerodynamic and gravitational forces with six degrees of freedom. Third, two spheres were dropped similar to the second case this time taking collisions between the two spheres into account. The force data compared with experimental data averaged an 8% error for 3.5 kPa suction out of the orifice, and 13% for 1.75 kPa suction out of the orifice, and 4% error for a 3.5 kPa suction case with second order dual time stepping. For the sphere drop cases, the desired behavior was known by experimentalists, and was achieved with minimal error. Testing on 8 to 96 processors with a 6.616 million grid point mesh demonstrated nearly linear speedup. Through the investigation, it was shown that the Chimera Grid Approach used with OVERFLOW is a valid choice for moving mesh applications.
UR - https://www.scopus.com/pages/publications/85067321743
U2 - 10.2514/6.2009-4120
DO - 10.2514/6.2009-4120
M3 - Conference article
AN - SCOPUS:85067321743
SN - 1048-5953
JO - Collection of Technical Papers - AIAA Applied Aerodynamics Conference
JF - Collection of Technical Papers - AIAA Applied Aerodynamics Conference
T2 - 27th AIAA Applied Aerodynamics Conference
Y2 - 22 June 2009 through 25 June 2009
ER -