I now have version 1.7 of my AAL77 FDR Decoder available on my web site along with new output files.
I have removed the DENSITY C TANK, DENSITY L TANK, DENSITY R TANK and DENSITY S TANK parameters and replaced them with the CORRECTED AOA parameter which has data stored in the same location but produces values that are close to the values for the INDICATED AOA parameter and therefore appear to be more sensible.
I have also added raw values for some parameters.
You can read further notes on the parameters here.
Warren.
Sorry, Warren,
There is something fundamentally wrong with with the Indicated AOA and Corrected AOA.
AOA has a
very specific meaning: the angle (in degrees) between the chord of the wing & and direction of free stream air past the wing.
And, whenever the plane is flying level or moving level (as when it is on takeoff roll), we KNOW what that number should be.
Whenever it is moving or flying level, the ACTUAL (i.e., corrected) AOA should be the Pitch Angle plus the Angle of Incidence (the angle of the wing chord with respect to the centerline of the plane).
Now, it turns out that the Indicated AOA is the angle that is given by the AOA vanes that are mounted on the "chins" of the plane. Further, the Angle of Incidence of the wings is not a constant from the wing root to the wing tip. The wing root has a higher angle of incidence than the wing tip does.
This variable camber give a couple of security effects: less lift from the outboard portions of the wing than from the inboard portions. This reduces the structural stress on the outboard portions of the wings, and reduces the size of the structural supports required. It also means that the inboard portions of the wing will stall first at high AOAs, and the outboard portion of the wing (where the ailerons are) will automatically be at a lower AOA, and therefore not be stalled. This means that the pilot will keep aileron authority thru the stall, and be able to control the plane & recover.
So, we know that the "Effective (i.e., average) Angle of Incidence" for the B757 is around 6°.
During take off roll, the FDR data shows that the Pitch Angle is 0°. This is perfectly normal. That means that, on the take-off roll, the actual AOA will be about +6°.
During level cruise flight, the FDR data shows the Pitch Angle is about +1.2°. This is a completely normal pitch angle for cruise, level flight. This means that, during level flight, the actual AOA is about 7 to 7.5°. This is also a completely normal, expected AOA for cruise flight.
This is what a B757 looks like when it is cruising in level flight.
The dashed lines are horizontal with respect to the ground. The plane is flying level, even though it nose is raised slightly (Pitch Angle = +1.5°). At this pitch angle, with level flight, the true AOA is about +7.5°. And you can also see the 6° Angle of Incidence.
Again, the -16° IAOA shown in the data is screwy. This is what a -16° AOA looks like. This plane will NOT fly horizontal.
I strongly suspect that this is getting redundant for you. And that you get the angles by now. Somehow the data is just nuts. I think it's time for an email to a Boeing engineer.
Tom