All Courses
All Courses
OBJECTIVE Simulation of Supersonic flow through a duct channel with sharp corners to observe the formation of shock waves. BOUNDARY CONDITIONS There are three types of boundary conditions used in CFD. When using a Dirichlet boundary condition, one prescribes the value of a variable at the boundary, e.g. u(x) = constant.…
Shouvik Bandopadhyay
updated on 13 Apr 2020
Leave a comment
Thanks for choosing to leave a comment. Please keep in mind that all the comments are moderated as per our comment policy, and your email will not be published for privacy reasons. Please leave a personal & meaningful conversation.
Other comments...
FULL SCALE COMBUSTION MODELLING OF A PORT FUEL INJECTION ENGINE
…
22 Jul 2020 08:09 AM IST
Week 7: Shock tube simulation project
…
24 May 2020 08:21 PM IST
Week 8: Literature review - RANS derivation and analysis
RANS LITERATURE REVIEW: DERIVATION OF RANS EQUATONS FOR TURBULENT FLUID FLOWS OBJECTIVE To apply Reynolds Decomposition to NS Equations and obtain the expression for Reynold's Stress …
21 May 2020 05:36 PM IST
Week 5 - Compact Notation Derivation for a simple Mechanism
Please Find the solution of the challenge attached.
20 May 2020 07:20 PM IST
Related Courses