I think Larry Flesner hit it right on the nose. Hope your HZ is adjustable

On Mon, Mar 30, 2020 at 5:56 PM Flesner via KRnet <krnet@list.krnet.org>
wrote:

> On 3/30/2020 9:35 AM, Dr. Feng Hsu via KRnet wrote:
> > The plane wants to go nose down from the first flight so we installed a
> > fixed trimtab on the elevator. Problem solved. I think we made the
> elevator
> > a bit to heavy, so the weight of the ellevator is forcing the nose
> > down.....I think.
>
> ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
>
> Stef,
>
> I don't think it is the weight of the elevator causing the nose down
> pitching, it is the angle of incidence of the horizontal stabilizer,
> which you can't change at this point.
>
> Consider this.  The early Cessna 170's (rag wing) did not have a
> balanced elevator. Setting on the ground ,with engine shut down, if you
> pulled back on the yoke to put the elevator at neutral and then let go
> of the yoke the elevator would drop to the down limit with a noticeable
> bang.  Air loads in flight tend to push the elevator to a more neutral
> position.
>
> A more relevant example is my KR.  It has a balanced elevator and on the
> ground the elevator tends to stay near the neutral position.  I can
> place my adjustable trim tab in the neutral position, take off and climb
> to altitude, push the nose over to cruise (150 mph), and if I let go of
> the stick, I will get a violent nose down pitch.  It is enough to throw
> things up off the seat  A bit of nose up trim removes the stick forces.
> In flight photos show the elevator still in the near neutral position so
> a very small change makes a big difference at higher speeds.  Once
> established in cruise I seldom touch the trim until I'm in the landing
> pattern or sometimes on a long letdown from altitude. That same setting
> is sufficient for takeoff and climb out and then adjust again for
> cruise.  One or one and one half degree more nose down angle of
> incidence on my horizontal stabilizer would make it more efficient in
> cruise.
>
> Bottom line.  If you're lucky you will set the horizontal stabilizer
> incidence to the correct angle for your normal cruise speed with an
> ideal C.G. location and the elevator at neutral. That would create the
> least amount of drag and give you the best speed.  Unfortunately life is
> not that simple.  Every other speed, power setting, and C.G. location
> would require a different angle of incidence on the horizontal
> stabilizer.  A number of aircraft designers did exactly that by making
> the horizontal stabilizer adjustable.  All the early Pipers through the
> TriPacer and the early C182's come to mind.  So, you have two options.
> One is a fixed tab to get zero stick forces at one given speed and C.G.
> location or two, some type of an adjustable tab or other device to
> relieve stick forces at different speeds.  Your KR is no different than
> any other airplane flying that requires pitch trim, adjustable or fixed,
> to relieve stick forces.
>
> One important thing to remember is if you use an adjustable trim tab
> make sure there is no slop in the system.  Any free play where the trail
> edge can move up and down can induce flutter and you don't even want a
> hint of that.  That's the reason I removed my steel cable operated tab
> setup and went with electric servo in the elevator.  With a coupling of
> only a few inches between the servo an the tab I was able to remove all
> free play in the system.  I recall the P51 that crashed at Reno
> developed a problem in the trim tab that caused flutter and that didn't
> end well.
>
> Second bottom line.  Don't worry about needing some pitch trim. All
> aircraft have that need.  If you can make C.G. changes to eliminate as
> much stick forces in cruise as possible, great.  That would be ideal.
> If not, go with what you have as long as it is safe.
>
> Larry Flesner
>
>
>
>
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