srara nina
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srara nina's Discussions

aerodynamics stability and control

Started this discussion. Last reply by Vladimir "Lazy" Khudyakov Jan 10. 3 Replies

how calculating static margin for fling wing configurationContinue

molding my master

Started this discussion. Last reply by srara nina Apr 9, 2012. 1 Reply

i want to make molding for my uav's master can you pleas tell me the stepsContinue


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Latest Activity

Vladimir "Lazy" Khudyakov replied to srara nina's discussion aerodynamics stability and control
"Use a XFLR"
Jan 10
Uwe Schuster replied to srara nina's discussion aerodynamics stability and control
"The static margin can be calculated from (AC-CP)/MAC where is the position of the aerodynamic center, CP is the Center of pressure, and MAC is the mean aerodynamic chord. All three are not so easy to calculate. You may want to use a free tool such…"
Jan 6

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stability and control

Comment Wall (2 comments)

At 5:57am on April 8, 2012, Ajienux said…

hi nina :)

At 4:55pm on April 26, 2012, Andrew Rabbitt said…

Hi there - static margin for a flying wing can be a bit tricky to explain, but Mr Deperrois does a good job in his paper

I'd really suggest downloading XFLR5 and having a play around with it.  There is at least one tutorial on YouTube to get you started to using it.

If you want to do hand calculations, have a look at this spreadsheet here

Good luck!

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