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martyn(at)flight.co.za Guest
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Posted: Mon May 08, 2006 2:31 am Post subject: Custom non STOL Elevator for CH 701 |
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Hello All,
We're waiting for our plans to arrive, and so as yet we have not started
building our plane. However, here in Johannesburg, South Africa, we are
about 6000 ft ASL. And the STOL performance figures quoted on the Zenith
site for the 701 will be very different up here.
I have heard from a 701 bulder here in South Africa, that the STOL
capabilities are a bit of an Overkill for South African flying conditions.
And that with the inverted elevator design, in a power off situation, the
nose tends to dip quite a lot.
So my question is this, Is it possible to Invert the inverted elevator?
What I mean to say, can we take the original elevator and invert it so
that the camber is on top! Thus making it a more traditional elevator?
Second question,
The leading edge slats are fixed, now, if i was to say, place the slats
flush with the wing, will that then give me the original NACA wing profile
that Chris Heintz used for this wing or is the NACA wing profile made up
of the Wing, the Slat and the Gap between the two?
Any comments and help will be greatly appreciated. I'm so looking forward
to starting on this plane. I've just gotta learn to be patient!
Kind Regards
Martyn Ward
www.Flight.co.za
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Max Johansson
Joined: 09 Jan 2006 Posts: 25 Location: Helsinki, Finland
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Posted: Mon May 08, 2006 3:39 am Post subject: Custom non STOL Elevator for CH 701 |
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Martyn
1. According to conventional thinking the upside-down elevator
is really there to prevent nose-dipping when using the 701
STOL capabilities. For a regular plane a flat horisontal tail
surface with a hinged elevator is enough to balance the aircraft.
2. In normal flight the 701 slat gap is not having an effect so
the profile is the overall profile. The gap geometry is rather
critical to adjust. The Pegastolg wing emplys moving slats in
order to have it both ways.
rgrds, Max, do not archieve
[quote] --
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_________________ Max
Max Johansson, Helsinki, Finland
Building a CH701SP-912S
on CZAW amphibian floats |
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bryanmmartin
Joined: 10 Jan 2006 Posts: 1018
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Posted: Mon May 08, 2006 5:25 am Post subject: Custom non STOL Elevator for CH 701 |
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The horizontal stabilizer on most aircraft has little or no camber, they use symmetrical airfoils or even flat surfaces. Remember, on a conventionallly configured airplane, the horizontal tail pulls down on the tail not up, so you would definitely not want the camber on the top. The inverted camber on the 701 allows the tail to provide more negative lift at very slow speeds in order to keep the nose up in slow flight.
-------------- Original message ----------------------
From: martyn(at)flight.co.za
Quote: |
Hello All,
We're waiting for our plans to arrive, and so as yet we have not started
building our plane. However, here in Johannesburg, South Africa, we are
about 6000 ft ASL. And the STOL performance figures quoted on the Zenith
site for the 701 will be very different up here.
I have heard from a 701 bulder here in South Africa, that the STOL
capabilities are a bit of an Overkill for South African flying conditions.
And that with the inverted elevator design, in a power off situation, the
nose tends to dip quite a lot.
So my question is this, Is it possible to Invert the inverted elevator?
What I mean to say, can we take the original elevator and invert it so
that the camber is on top! Thus making it a more traditional elevator?
Second question,
The leading edge slats are fixed, now, if i was to say, place the slats
flush with the wing, will that then give me the original NACA wing profile
that Chris Heintz used for this wing or is the NACA wing profile made up
of the Wing, the Slat and the Gap between the two?
Any comments and help will be greatly appreciated. I'm so looking forward
to starting on this plane. I've just gotta learn to be patient!
Kind Regards
Martyn Ward
www.Flight.co.za
|
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_________________ --
Bryan Martin
N61BM, CH 601 XL, Stratus Subaru.
do not archive. |
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ggower_99(at)yahoo.com Guest
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Posted: Wed May 10, 2006 8:30 pm Post subject: Custom non STOL Elevator for CH 701 |
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Hello Martyn,
Welcome to the list, Please NO!
I fly from 5,000 to 7,200 ft ASL strips here and the 701 flys PERFECT.
Please DONT MODIFY ANY airplane unless you are qualified to do it... Dont pay atention to "hangar experts" dont get killed and damage the image of a great airplane and the Sport just because one smart guy opinion.
I once heard: You want to make an airplane designer have a heart attack? Modify his design
I will advice you: Before building ANY airplane, learn and read all possible literature from "secure" source and if possible get a test flight and or some videos of the airplane.
The 701 is just perfect as designed, for the intendend way to fly. No need a STOL airplane?, or want a faster one? Or you have good landing strips?, then chose another airplane.... the 601 for example.
Hope this helps, not mad at all, just frightened that you can get hurt... No ofence intended.
And yes, all newbie builders (I was one of them 20 years and 3 projects ago). think that they are smarter than any designer... Every modification for simple as it looks can ADD about 100 hrs to the building time of the project... been there done that...
Saludos
Gary Gower
701 912S
Flying from Chapala, Mexico
martyn(at)flight.co.za wrote:
Hello All,
We're waiting for our plans to arrive, and so as yet we have not started
building our plane. However, here in Johannesburg, South Africa, we are
about 6000 ft ASL. And the STOL performance figures quoted on the Zenith
site for the 701 will be very different up here.
I have heard from a 701 bulder here in South Africa, that the STOL
capabilities are a bit of an Overkill for South African flying conditions.
And that with the inverted elevator design, in a power off situation, the
nose tends to dip quite a lot.
So my question is this, Is it possible to Invert the inverted elevator?
What I mean to say, can we take the original elevator and invert it so
that the camber is on top! Thus making it a more traditional elevator?
Second question,
The leading edge slats are fixed, now, if i was to say, place the slats
flush with the wing, will that then give me the original NACA wing profile
that Chris Heintz used for this wing or is the NACA wing profile made up
of the Wing, the Slat and the Gap between the two?
Any comments and help will be greatly appreciated. I'm so looking forward
to starting on this plane. I've just gotta learn to be patient!
Kind Regards
Martyn Ward
www.Flight.co.za
---------------------------------
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jean-paul.roy4(at)tlb.sym Guest
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Posted: Thu May 11, 2006 2:33 am Post subject: Custom non STOL Elevator for CH 701 |
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Very wise advise here
Jean-Paul Roy
do not archive
---
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