![]() |
|
|
|
#1
|
|||
|
|||
|
Quote:
|
|
#2
|
|||
|
|||
|
I'm unsure if the graphics match the FM (i.e. seeing or not the slats deployed currently makes any difference).
Anyway, I noticed yesterday that while powering up the 109, the slats started to pop out and in, out and in (no pun intended). Since they move relative to the air speed, the slats should be out when the plane is in a stopped state on the ground which seems not to be the case. |
|
#3
|
|||
|
|||
|
Quote:
(this Sim is really great) |
|
#4
|
|||
|
|||
|
Quote:
|
|
#5
|
||||
|
||||
|
How can she be shy if she is a slu..
Oh.. wait one.. slats! My bad.. thought you were talking about something else!
__________________
Theres a reason for instrumenting a plane for test..
That being a pilots's 'perception' of what is going on can be very different from what is 'actually' going on. |
|
#6
|
|||
|
|||
|
109 E plane description says they should extend at 180 km/h.
|
|
#7
|
|||
|
|||
|
Here are the values the RAE determined in Flight test Source AVIA 6/2394 BF109E Evaluation
![]() These are 1G values. So slat deployment under G will be Whatever number you use (ASI or trailing) from these x SQR of the G Last edited by IvanK; 11-01-2011 at 07:57 AM. |
|
#8
|
||||
|
||||
|
Quote:
|
|
#9
|
|||
|
|||
|
So how about posting some here for us to peruse. The more data we have the better. Ideally Slat development AOA's .
Last edited by IvanK; 11-01-2011 at 12:14 PM. |
|
#10
|
|||
|
|||
|
Quote:
Regardings Crumpps chart, "Spaltklappen" and "Spreizklappen" are two different types of flaps, not leading edge slats. The slats don't open gradually. But from that polar and the RAF test, it should be easy to derive the AoA of ~ 8° at which they bang open. |
![]() |
|
|