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Showing results 1 to 5 of 5 Search took 0.00 seconds. Search: Posts Made By: agd

Forum: Main CFD Forum February 25, 2010, 11:27

Replies: 17 does anybody believe that we can estimate the pressure around a wing without solving Views: 2,005 Posted By agd If I had a dollar for every time I have heard... If I had a dollar for every time I have heard some variation of this theme, I could have retired years ago. Look, either you are using a DATCOM-like approach, involving copious amounts of empirical...

Forum: Main CFD Forum February 25, 2010, 10:48

Replies: 17 does anybody believe that we can estimate the pressure around a wing without solving Views: 2,005 Posted By agd So show us instead of just repeating how "stupid"... So show us instead of just repeating how "stupid" we are. Put up or shut up. Show me how you get the pressure around a NACA 0012 airfoil at a 15 deg. AOA and a Re = 6 million - just the equations...

Forum: Main CFD Forum February 25, 2010, 10:39

Replies: 17 does anybody believe that we can estimate the pressure around a wing without solving Views: 2,005 Posted By agd Yes - I too would be interested in the governing... Yes - I too would be interested in the governing equations you recommend we use.

Forum: Main CFD Forum February 25, 2010, 09:54

Replies: 17 does anybody believe that we can estimate the pressure around a wing without solving Views: 2,005 Posted By agd So you are dismissing the governing equations,... So you are dismissing the governing equations, and then appealing to the same governing equations - now I'm wondering if I'm the confused one.

Forum: Main CFD Forum February 24, 2010, 22:46

Replies: 17 does anybody believe that we can estimate the pressure around a wing without solving Views: 2,005 Posted By agd So I'm confused - how do you propose getting the... So I'm confused - how do you propose getting the force? What if the airfoil flow is separated? What if friction drag is important? You rule out using the Euler equations, the NS equations, and...

Showing results 1 to 5 of 5

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