Hey everyone, Thanks for all your replies. @JRMacGregor: That was a good idea, to ask the university. Thank you so much. :) @conceptia: What...
Hey, thanks for the reply. :) I am interested more in Hydrodynamics/Ship Hydromechanics (you know, like seakeeping, maneuvering, resistance and...
Hey everyone, I just finished my undergraduate degree (B.Tech(Hons)) in Ocean Engineering and Naval Architecture. I wish to pursue an MS in...
Hi everyone! I am trying to simulate a small fully-submerged ellipsoid rotating about a point. For the rotating arm simulation. I have defined a...
Hey everyone! I have been trying to mesh this geometry for a really long time now.. :( (http://picasaweb.google.com/lh/photo...eat=directlink)....
Hey everyone! :) This is me troubling you with yet another (stupid) doubt. Hope you all will again come to my rescue. I am trying to export...
Thank you everyone. I shall keep this in mind whilst I am doing the analysis. :) Thanks a lot.
I had one other question too. If you all could please take out time to visit this thread, I'd really appreciate it. Thank you....
Hi! I would like to know that which one is a better software for doing CFD analysis of an AUV: Solidoworks (COSMOSFloWorks) or FLUENT? I...
Hey, thanks. But I dont think I'll trouble you with all that. I managed to get myself a copy of michlet. :) I shall see what I'm able to do with...
Thank you so much everyone. @daquiri: I dont have a picture at the moment of the vehicle, but I can tell you that it looks like an airplane...
Anyone? Can you just tell me if Maxsurf would be enough to do the calculations? I mean to ask, is it reliable? Even this would be enough. Thank you.
Hey Everyone! I am working on a small diving vehicle at IST, Lisbon. I have the shape of the vehicle modeled in SolidWorks. Now I wish to carry...
Hmm.. Thanks Rick I'll think about it. :)
Also Rick I wanted to ask you, What happenes to a NACA 2410 foil if the angle of attack is 180 degrees? I know the lift coefficient will be...
Ok..thanks Rick. And one more thing Rick. I was just playing with the values in JavaFoil. I found one interesting thing with the airfoil cross...
Dear Rick, I am using this formula to calculate the Reynolds number. Is this correct? Rey. Num. = density*velocity*chord length/abs....
Thank you Rick. :)
Rick, And also if I change the dimensions of the Aerofoil to Span = 8 cm Chord = 2 cm How will the Reynolds number change? Can you tell me how...
And the stall model: CalcFoil And Transition model : Eppler
