9 Questions 5 Answers 0 Followers
Questions related from Samuel Luis
Are the equations of Fay and Riddell embedded in Fluent or do they have to be imported using a UDF?
02 February 2018 7,898 3 View
As usually the trend is a Courant number (CFL no) can only be used for a Transient( Unsteady) flow condition. Thank you in Advance.
02 February 2018 2,016 6 View
I am not clear whether to use a Pressure Based Solver or a Density Based Solver. Thank You in Advance
10 October 2017 2,711 18 View
Typically at Hypersonic Free Stream Mach numbers and to capture the flow separation and reattachment in the afterbody flow of a re-entry capsule
10 October 2017 792 3 View
Generally after the calculation has been run and during post processing of results in either FLUENT or CFD-POST.
09 September 2017 2,375 3 View
I would like to know the boundary conditions for simulating the above .
09 September 2017 1,546 2 View
Typically a 3D adaptive grid for simulating the afterbody flow of a reentry capsule.
09 September 2017 986 0 View
Typically Hypersonic Afterbody flows involving blunt body re-entry vehicles(spacecraft) with an angle of attack and flow separation taking place in the afterbody flow.
05 May 2017 9,964 4 View
These include hypersonic re-entry flows where bow shocks or detached shocks are formed.
04 April 2017 9,298 2 View
