Video quality and accurate results in CFD the thing which I like most... Will u plz do video on the CFD analysis of heat transfer by radiation and plz provide temperature profile 🙏🙏🙏
I watched that videos but I didn't see temperature profile anywhere which is very necessary for us I request you to add temperature profile for radiation especially or make another video ( I saw your this video of venturimeter in which I wanted to see pressure and velocity variation along the flow so tysm for that I appreciate your work very much 🙏)
Hi I have a question about rocket tech. Spacex Stage1+Stage2+Fuel weight is 4500tons. I dont believe any number of rocket engine can lift that weight and the thin fuselage can hold that fluid without failing. I would like to know your opinions about these rocket structures. Thanks.
Sir, i have sent mail to you regarding the flow simulation...i have attached result..please help me what wrong i have done in simulation..kindly guide me sir
sir if my inlet p is 20 bar then should i enter in initial condition as 20 bar and temp say 40°c... what will be my boundary conditions at inlet and outlet
Inlet Boundary conditions should be as per actuals. It is user dependant and if there is any exit it should be having environmental pressure or atmospheric pressure
@@CFD_GUIDE thank you sir..today evening after my office work i will do this and analyze the results as per your recommendations. sir i want to contact you through mail is that possible sir?
Video quality and accurate results in CFD the thing which I like most...
Will u plz do video on the CFD analysis of heat transfer by radiation and plz provide temperature profile 🙏🙏🙏
I have already made some videos containing radiation
I watched that videos but I didn't see temperature profile anywhere which is very necessary for us I request you to add temperature profile for radiation especially or make another video ( I saw your this video of venturimeter in which I wanted to see pressure and velocity variation along the flow so tysm for that I appreciate your work very much 🙏)
Hi I have a question about rocket tech. Spacex Stage1+Stage2+Fuel weight is 4500tons. I dont believe any number of rocket engine can lift that weight and the thin fuselage can hold that fluid without failing. I would like to know your opinions about these rocket structures. Thanks.
Thanx
Sir, i have sent mail to you regarding the flow simulation...i have attached result..please help me what wrong i have done in simulation..kindly guide me sir
sir if my inlet p is 20 bar then should i enter in initial condition as 20 bar and temp say 40°c... what will be my boundary conditions at inlet and outlet
Inlet Boundary conditions should be as per actuals. It is user dependant and if there is any exit it should be having environmental pressure or atmospheric pressure
@@CFD_GUIDE thank you sir..today evening after my office work i will do this and analyze the results as per your recommendations. sir i want to contact you through mail is that possible sir?
No issues at all. Send an email
@@CFD_GUIDE ok sir