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flightnse wrote:QUOTE (flightnse @ Jun 30 2008, 11:32 AM) <{POST_SNAPBACK}>i would say about 270
???
Anyway, the theory is this:
The AoA of the airfoil (or wing) needs to change as airspeed changes to maintain level flight... as speed is reduced, we increase the AoA to compensate (airflow over the wing decreasing = decreased lift, increasing AoA = increases lift and vice versa)... now if we expand the diagram to include the entire aircraft:
It stands to reason that if the AoA of the wing is changing, the AoA of the rest of the aircraft (including the prop) must also change... as everything is fixed... so the AoA of the prop must be changing.
I wonder if the same applies to the trike in FSX, as the wing is actually hinged, so you can alter the AoA of the wing independently from the rest of the trike?
Figured I would go with the logic argument, as I cannot be bothered trying to draw vectors
EDIT: Man, went and did some reading on this... and trying to understand the theory is making my head hurt (I got up early to watch the football this morning, so I'm not very with it at the moment!)
But it is all to do with Rotational Velocity and Forward Velocity determining the relative airflow and hence AoA of the prop...
If you change either the Rotational Velocity (increasing or decreasing RPM), or the Forward Velocity (speed brakes? or dropping flaps maybe) the relative airflow (and hence AoA) changes... as the triangle shape is changing...
Thx for forcing me to look this up... CPL Principles of Flight is coming up soon...Last edited by HardCorePawn on Mon Jun 30, 2008 1:36 pm, edited 1 time in total."Son, we are about the break the surly bonds of gravity, and punch the face of God." -- Homer Simpson
flightnse wrote:QUOTE (flightnse @ Jun 30 2008, 01:45 PM) <{POST_SNAPBACK}>what do you mean ???
Mate... probably a bit of overkill quoting my entire post... just to say WTH?
That is a somewhat complicated explanation as to how/why the Angle of Attack (or AoA), of a fixed pitch prop, varies with changes in airspeed and/or rotational velocity of the prop. What happens is that the relative airflow across the blade changes, but the chord line of the prop blade remains constant. As with a wing, the AoA is the angle between the chord line and the relative airflow.
So if the relative airflow is changing, the AoA must change as well."Son, we are about the break the surly bonds of gravity, and punch the face of God." -- Homer Simpson


HardCorePawn wrote:QUOTE (HardCorePawn @ Jul 2 2008, 09:50 AM) <{POST_SNAPBACK}>I actually just realised that according to the original rules, you're not supposed to participate for 3 goes after you've got one right... so I will ask
my question and then lurk for a while...
Oh yeah.....doh... Guess I'm out for a while too then




HardCorePawn wrote:QUOTE (HardCorePawn @ Jul 2 2008, 09:50 AM) <{POST_SNAPBACK}>I actually just realised that according to the original rules, you're not supposed to participate for 3 goes after you've got one right...
Now while Travnz figures out another diabolical question...
how about doing a little penance, and explaining all that jargon?Last edited by Charl on Thu Jul 03, 2008 9:06 pm, edited 1 time in total.

Charl wrote:QUOTE (Charl @ Jun 30 2008, 06:52 PM) <{POST_SNAPBACK}>Now if you two have finished with the physicslecture, HCP has a turn now.
Minus five marks if you need an aeronautical degree to answer the question...
HCP take MINUS FIVE MARKS...
And add 'em back for the last line, for showing you do have a sensayumour.Last edited by Charl on Fri Jul 04, 2008 1:30 pm, edited 1 time in total.
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