Posted by: funked =925 CABS=
Message: Ik - I'm not sure what you are observing - does the Yak
keep rolling more after you release the stick, or is it slow to initiate
the roll?
The following discussion covers either case.
Some definitions:
T (lb-ft) = Roll moment from ALL aerodynamic forces.
I (lb-ft-s^2) = Moment of inertia about roll axis.
alpha (1/s^2) = angular acceleration about roll axis.
Governing Equation:
T = I * alpha
Ik, you are observing alpha with your eyes, and estimating T from your
control inputs.
No doubt your alpha estimates are pretty good, but T is hard to do for
two reasons:
1. Any two planes have different control systems. A given stick deflection
will result in different roll moments on the aircraft
2. Note that T is not just the roll moment due to aileron deflection
- it also accounts for opposing forces due to drag, etc. - those forces
that tend to slow a plane's rate of roll once the stick is released. These
forces oppose the direction of roll and are generally proportional to roll
rate.
So my theory is that either/both:
A. The Mosquito has a greater aileron "gain" than the Yak,
i.e. more
roll moment for a given stick deflection. Think of the FW190 vs. the
Zeke.
B. The Yak has lower aerodynamic resistance to rolling. So once you release
the stick, it keeps rolling, giving the impression of large inertia. Kind
of like the P51's behavior.
Or,
C. Anticommunist forces have conspired to restrain the dominance of the
most badass dogfighting machine of the late-war era.
funked =925 CABS=
(design engineer, aircraft actuation systems)
Posted by: nrts - =4th FG=
Message:
: Anyone else notice that the Mossie has less roll inertia than the
Yak? Let's see, the yak has TINY wings, and the guns are in the nose. The
Mossie has a large wingspan, and on top of that has two engines on the wings.
This makes no sense to me? Am i too feeble minded to realize the explanation
to this paradox?
: ik
Well you've got your roll inertia and it is dominated by the polar moment
of the wings which depends on the distributed mass of the wings, i.e., guns
out on the wings (long moment arm) vs. guns on fuselage (short moment arm).
This is the actual roll moment of the vehicle.
But, then you have the "apparent" roll moment which is influenced
by control surface area (aileron area). For example, you correctly state
that the Mossie should have a hefty roll moment and I agree. The apparent
roll moment which manifests itself as roll-rate is determined by the ratio
of the torque the ailerons can command about the roll axis to the resistance
to roll or roll moment. Yeesh! What I'm saying is that the Mossie must have
lots of aileron area for such a low resultant or apparent roll inertia.
That should translate to large drag forces when these surfaces are actuated
meaning that this airframe should bleed energy in a turn like no other.
Hows that for an Electrical Engineer? :)
-nrts- |