Name | Modified | Size | Downloads / Week |
---|---|---|---|
Parent folder | |||
capsule_grid.f90 | 2023-05-26 | 197.2 kB | |
README | 2023-05-25 | 6.7 kB | |
build | 2021-07-13 | 936 Bytes | |
capsule.sh | 2019-10-31 | 2.3 kB | |
capsule.inp | 2018-05-13 | 15.4 kB | |
heatshield-generator.glf | 2013-12-24 | 3.9 kB | |
capsules.f90 | 2013-12-24 | 35.4 kB | |
Capsule_Grid.pdf | 2013-12-05 | 12.1 MB | |
2D-forebody.glf | 2013-08-19 | 2.1 kB | |
2D-full-body.glf | 2012-01-03 | 2.0 kB | |
NosePatch61B.p3da | 2007-12-14 | 214.9 kB | |
Totals: 11 Items | 12.6 MB | 0 |
CAPSULE_GRID performs automated discretization of analytically-defined generatrices for typical (and not-so-typical) axisymmetric capsules such as 70-degree sphere/cones with optional aft bodies. For zero angle of attack cases, related procedures produce the associated initial volume grid needed for flow field calculations. Non-analytic input generatrices are also handled. For angle of attack cases, a surface grid is also produced, with the singular point region at the nose (and aft body if present) replaced by morphed quadrant patches. Volume grids may likewise be produced with related procedures. Please see Capsule_Grid.pdf and the header of capsule_grid.f90 for further details. 06/30/2016 " " A new option in CURVDIS to work with adjusted curvatures that are artificially broadened onto flat/low-curvature segments appears to be good for analytic geometries but unreliable for input generatrices of unknown quality/precision. New controls flat_blend_fore & flat_blend_aft allow this option to be suppressed. It was prompted by a clear need to resolve heat flux spikes at the shoulder better by spreading the tight shoulder grid spacing forward onto the conical flank. This should work for Apollo- type spherical sections too (large radius/low curvature) given that we work with normalized geometry during curvature-based redistribution. Namelist controls are now printed to standard output. 10/27/2016 " " Aft-end stretching towards the symmetry axis in the generatrix is undesirable. 3D surfaces replace this region with uniform quadrants. Therefore, do similar to the generatrix, using ni_regrid_aft_body and a heuristic number of uniform points at the end. 04/05/2018 " " An indexing error was found in the above uniform redistribution of the aft generatrix end. 08/23/2018 " " The analytic aft body case's forcing of uniform spacing away from the aft stag. point was not right because x/rgen(:) was being reused for the aft body (starting from 1, not numi_forebody). 09/25/2019 " " Rerunning on the capsule-on-a-sting analytic case gave troubling aft-body results, traced to interference of the vertex-detection scheme in CURVDIS with the (later) scheme for broadening the curvature-based shape function on to flat or low-curvature segments. Better blending on to such segments (and either side of sharp corners) is highly desirable, but fraught with potential difficulties due to the unavoidable heuristics. 10/30/2019 " " Introduced nblend_fore_aft control. The default of 8 can mean poor results going from tight spacing on the shoulder to larger spacing on the aft cone. Spreading the blending over more points should help. 11/30/2019 " " A pitot tube case from Dinesh revealed that an input generatrix did not have the scale factor applied as for analytic cases. Rectified now. 01/17/2020 " " Minor tweaks to the "umbrella" case for it to work in the absence of a rounded shoulder aft of the underlying cone and a nose cap larger than that cone. 06/17/2021 - " " Parachute cones with different TPS material have 06/25/2021 required splitting of aft body surface patches for BC purposes (catalycity). The dimensions either side of the split need to be of the form 4n + 1 in order for the initial fine grid to be coarsened once for production use (221) and coarsened again for grid sequencing (441|442) during an initial unaligned grid solution. Introduced x_parachute_cone control. Patch dimensions either side of this x > 0. will be adjusted to the closest 4n+1 form as well. The number of surface patches becomes 16. 09/07/2021 - " " New asymmetric and lower_generatrix inputs 09/29/2021 enable handling of an asymmetric forebody with an optional axisymmetric aft body, as prompted by Mars Sample Return Lander configuration V21. 10/29/2022 " " The parachute cone split option, which forces point counts either side to be 4n + 1, means there is likely to be redistribution (splining) across the PC lid corner. Now we look for such a corner and preserve it exactly. The same may be needed upstream of the split, although the shoulder step corner of SRL DAC-2.2 seems to be unaffected. 05/24/2023 The 10/29/22 extension to preserve a parachute lid corner during redistribution associated with capturing x_parachute_cone was thwarted by a corner at a shoulder step combined with a less sharp PC lid corner (SRL Rev B having a rounded lid). This idea has been abandoned. If the capturing of x_parachute_cone loses geometry features, the only work-around is to provide a generatrix with the desired points and point counts, and to ensure the generatrix is retained through proper choice of numi_forebody and nu i_aft_body. (Sorry.)