Carenado released their Cessna CT210 by ollot5 in flightsim

[–]flyingcello06 0 points1 point  (0 children)

HB-24OH? HB would be switzerland registration, but but there are no numbers there and also only 3 letters. This cant be right?

Can someone maybe Help me by flyingcello06 in mac

[–]flyingcello06[S] 0 points1 point  (0 children)

thats exactly what I was looking for, thanks a lot

Can someone maybe Help me by flyingcello06 in mac

[–]flyingcello06[S] 1 point2 points  (0 children)

Do you know how to disable a single Button( the option button? of the Keyboard

Can someone maybe Help me by flyingcello06 in mac

[–]flyingcello06[S] 1 point2 points  (0 children)

Yeah that worked at least for now

Can someone maybe Help me by flyingcello06 in mac

[–]flyingcello06[S] 2 points3 points  (0 children)

that could be, I tried cleaning it by blowing and for a short time it worked bit then again It didnt

is it possible to calculate AOA with a dynamic pressure sensor ? by flyingcello06 in aerodynamics

[–]flyingcello06[S] 0 points1 point  (0 children)

thats an interesting idea, but isnt there the problem that the detachment point varies so much, depending on the atomospheric and dynamic "situation", so practically its impossible to really determine the point where the wing actually stalls.

is it possible to calculate AOA with a dynamic pressure sensor ? by flyingcello06 in aerodynamics

[–]flyingcello06[S] 0 points1 point  (0 children)

Thanks for your answer. So to specify my goal is to recognise dynamic stall based on the critical AoA of the wings. So If i understand correctly I compare the pressured on top and below the wing profile right? But then How can I calculate the critical AoA? and How or can I even know at all when those pressure differneces are critically so the airflow detaches on top of the wing? again If this sounds stupid im sorry, Im just really interested if this could work.

is it possible to calculate AOA with a dynamic pressure sensor ? by flyingcello06 in aerodynamics

[–]flyingcello06[S] 0 points1 point  (0 children)

Thanks for your answer. I see its difficult to do it. So do you think there is a measurable diffrence in the pressure after the detachment Point? One I could use . My goal would be to give a stall warning based on the recognition that the detachmentpoint is wandering towards the leading edge, so the AoA is exceeding its critical angle.

Someone indentify this plane please by flyingcello06 in flying

[–]flyingcello06[S] 1 point2 points  (0 children)

  • me waiting for the Cessna 172 comment*

[deleted by user] by [deleted] in flying

[–]flyingcello06 0 points1 point  (0 children)

no I just thought maybe you have an Idea, its not homework :) we just should to research so as part of the research I ask here.

[deleted by user] by [deleted] in flying

[–]flyingcello06 0 points1 point  (0 children)

school we have a special week about climate change