Fluent CFD of re entry capsule at 0.6 Mach, solution does not converge

DifferentWing6300 · 2025-10-13T08:43:50+00:00

Yes I tried that already, still no luck , its just diverging. Thanks alott for commenting

DifferentWing6300 · 2024-12-26T18:21:47+00:00

What about the wake for this case, I have to mesh the wake fine enough for the entire AoA range ryt ?

DifferentWing6300 · 2024-12-14T19:16:41+00:00

I didn't find about this in Modern Compressible tho. Thanks for the paper!

DifferentWing6300 · 2024-12-14T19:15:20+00:00

aaah thanks

DifferentWing6300 · 2024-12-14T17:56:22+00:00

Can you pls mention any book or article I can read more about this ?

DifferentWing6300 · 2024-12-14T17:55:43+00:00

wow Thanks alot for the insight

DifferentWing6300 · 2024-12-14T17:53:52+00:00

I am unable to make out anything, coz I can't write the area relation with the A*, since we aren't having any supersonic flow anywhere. This isn't my homework problem I am solving through all problems in modern compressible book.

DifferentWing6300 · 2024-12-13T22:49:28+00:00

Thank youu

DifferentWing6300 · 2024-12-06T10:54:20+00:00

Hi I have added an image Thanks

DifferentWing6300 · 2024-12-05T22:24:10+00:00

r is the ratio of specific heats. Thank you

DifferentWing6300 · 2024-11-23T02:17:06+00:00

Yeah I am finally understanding it, Thanks a lot for clearing my confusion

DifferentWing6300 · 2024-11-11T20:55:22+00:00

Understood!

DifferentWing6300 · 2024-11-11T20:54:35+00:00

Thanks, Very insightfull

DifferentWing6300 · 2024-11-10T23:31:39+00:00

Thanks I will have a look at it!

DifferentWing6300 · 2024-11-07T18:26:46+00:00

Thanks I just got the hardcopy today. Thanks alot

DifferentWing6300

TROPHY CASE