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- Klipkopwildlife
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Do it now, you may never get another chance
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- Eric
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The problem is - it is weakest where you need it to be strongest!
The high-stress area when considering weight-carrying/g-loading - is the mid-section, where most designers put the wing-joining tube!
With a shape like that, you cannot have a straight tube or bar, so all the stress is carried on a couple of wing-locating tabs and the flying wires.
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When it comes to Vee-tails, again you have no structural strength - and a compromised vertical vs horizontal area wing-plan. If you compress the verticals somewhat, and flatten the curve round to the horizontal, you are back to the existing T-tail configuration we are already using. That also has it's own problems. To make the joint between the vertical fin and the horizontal tail, you need a good joint. (usually a bolt or two, so it can't rotate!) and that imparts a twisting stress to the fuselage in anything but a perfect landing.
And - depending on the moment arm (the length of fuselage between main and tailplanes), the aircraft can get into a nose-high attitude where the stalled mainplane is totally masking the tailplane, leaving the pilot with zero pitch control until the ground gets in the way - whereas a 'normal' tailplane would be below the disturbed air of the stalled wing, which would automatically push the nose down.
if you are calm and collected when all about you are going berserk - you've missed something important!
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- Eric
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if you are calm and collected when all about you are going berserk - you've missed something important!
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- Magpie
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And being a biplane it is stronger.
To me both the conventional tail & the T-tail both have wobbly fins.
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- Quorneng
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i would also suggest the wing has no joiner but is built up in one piece that includes a section in the fuselage. It is then bolted down.
Advantage? Yes. it means as a biplane you can do away with the cabane struts but at the expense of considerable manufacturing difficulty.
Now if you are flying at 400+mph there is a drag advantage if the wing joins the fuselage at 90 degrees, like the inverted gull wing of the Chance Vought Corsair fighter, although in that case it also allowed the undrcarriage to be a bit shorter and still give ground clearance for the biggest ever fighter prop so was deemed worth the construction difficulty.
The same really applies to a V tail. A straight V is easier to construct than a curved one so there has to be a good reason to go to the trouble. Most V tails have full length control surfaces to generate the required effect. A working curved control surface would be a mechanical nightmare.
On one of my planes I use a V tail so it is less likely to get damaged in a long grass belly landing. I selected a fairly wide angle V to give adequate elevator authority but I found it then lacked sufficient tail vertical area so had marginal directional stability in a turn. The simple solution was a "compound" V with vertical bits at the tips of the V.
It worked very well for my particuler set of circumstances.
I hope this helps.
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if you are calm and collected when all about you are going berserk - you've missed something important!
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if you are calm and collected when all about you are going berserk - you've missed something important!
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- Eric
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www.bbc.co.uk/news/articles/cr5plvn0j5ro
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www.bbc.co.uk/news/articles/cj9p8rvl0d0o
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- Quorneng
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They have been flying the Hawk T1 since 1980 that's 26 years. There are some airliners older than that but the Red Arrows Hawks have been doing high g aerobatic manoeuvres regularly ever since.
The end date for the Red Arrows Hawks is 2030. I wonder how many planes they will be using in their aerobatic displays by then!
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- Eric
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- Klipkopwildlife
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We went to 2 Game reserves, one which BB knows (Marakele) and another one, Pilanesberg. A bit of 'memory lane' stuff since Mary remembers very little of the more recent Pilanesberg stuff but all the hours that she and her friend Brenda put in 40 years ago!
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- THE BLACKBIRD
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