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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 13:51 
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its funny as cars don't have keys anymore, its all push button.

Username Protected wrote:
A key?
Who wants a key in a jet? That is so piston thinking mentality.


That is knowing your customer. What is so special about having to push a button/toggle versus turn a key?

Tim

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 14:30 
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its funny as cars don't have keys anymore, its all push button.



I've got this stupid fob for my Ram. It has buttons on it for lock, unlock, start and panic that have never been pressed. I stick my hand in the handle and the doors unlock. I press the button and it starts. If I want to remote start it, I do so with an app on my phone. Why can't that stupid fob be the size and thickness of a credit card so I can put it in my wallet?


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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 14:31 
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Username Protected wrote:
its funny as cars don't have keys anymore, its all push button.


Actually, RFID for the door locks and button to start/stop. But the RFID depends on constant power draw and the alarm system. Considering the time people let planes sit and already hook the battery up to a minder not sure this would be a good solution for a plane. Besides, this is fairly recent for main stream cars.

Tim


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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 14:32 
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Username Protected wrote:
its funny as cars don't have keys anymore, its all push button.



I've got this stupid fob for my Ram. It has buttons on it for lock, unlock, start and panic that have never been pressed. I stick my hand in the handle and the doors unlock. I press the button and it starts. If I want to remote start it, I do so with an app on my phone. Why can't that stupid fob be the size and thickness of a credit card so I can put it in my wallet?


I used to have a MB S600 (bought it used, no way could I afford it new) which had one. About twice the thickness of a credit card.

Tim

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 14:41 
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Joined: 12/03/14
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You're still forgetting about the vertical stab that isn't there. Yes, a V-tail does induce more drag than an elevator for a given amount of down/up force. But, it doesn't induce more drag than an elevator AND a vertical stab.

I think you are wrong about that. The total wetted area of the SF50 tail is substantially more than a conventional tail including the fin. And that is before you add pitch trim drag effects of the V tail.

If a V tail was more efficient, you would see them on airliners where every tiny improvement is desired. You don't see that at all.

The V tail exists for only one reason, to make room for the single jet exhaust. It is aerodynamically inferior to a conventional tail which is why the conventional tail is conventional (and used by Cirrus on SR20/22).

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 14:48 
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Username Protected wrote:
So it can flare.

Other airplanes with lesser control surfaces flare just fine.

How can they do that?

Their conventional horizontal surface is applying force directly in the up or down direction, not some percentage less caused by the angled surface of a V tail.

Quote:
Making a surface that can deflect 12" doesn't add any more drag than a surface that can deflect 6".

Yes, it does.

The surface can't deflect 12 inches and provide good control, parts of it stall or you get air burbles and vibration (like some big flaps). So smooth and relatively proportional controls means limits on control surface deflection. If you need more force, you need more surface. More surface is larger hinge line, more weight, larger balance weights, etc, which all effect efficiency. The hinge line is a notable cause of surface inefficiency since it represents both a break in the airfoil shape and a potential air leak from one side to the other (hence the desired for gap seals which don't always work out in practice).

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The drag comes from actually deflecting them, which won't be done at speed. Nobody is going to be full deflecting anything at 300kts and FL280.

No, but you will have partial deflection for trim with varying CG and speed. On a V tail, some of the lift is lost in a yaw fight and doesn't help trim the airplane in pitch.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 15:56 
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Username Protected wrote:
If a V tail was more efficient, you would see them on airliners where every tiny improvement is desired. You don't see that at all.


Everyone who flies a Bonanza knows that V-tails are more efficient.


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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 16:18 
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Username Protected wrote:
Everyone who flies a Bonanza knows that V-tails are more efficient.

Unfortunately, the laws of physics are not determined by a vote.

One has to ask why Beech made EVERY airplane after the 35 less efficient by using a conventional tail.

Mike C.

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 16:30 
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Username Protected wrote:
Everyone who flies a Bonanza knows that V-tails are more efficient.

Unfortunately, the laws of physics are not determined by a vote.

One has to ask why Beech made EVERY airplane after the 35 less efficient by using a conventional tail.

Mike C.

When a few tails rip off, that is bad for business.

Lose the absolutes Mike....
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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 17:02 
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Username Protected wrote:
Everyone who flies a Bonanza knows that V-tails are more efficient.

Unfortunately, the laws of physics are not determined by a vote.

One has to ask why Beech made EVERY airplane after the 35 less efficient by using a conventional tail.

Mike C.


General consensus was cost. The V-Tail was significantly more to produce. It was not worth going through certification again to make the design a lot cheaper to produce.
Further, the V-Tail was also dealing with some bad press at the time; which increased the doubt of eventual cost recover.
Lastly, Beech had a conventional six place airplane in production.

Tim

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 17:05 
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Pretty hard to argue the facts....
Mike isn't the one designing airplanes the last 40 plus years, yet no one has made a production plane with a non conventional tail over that time period. Seems that all those thousands of engineers at however many aircraft manufactures use the same math he does and come up with the same answers....

If the V tail was more efficient, Beech would still be making it and so would everyone else.


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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 17:12 
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Username Protected wrote:
Pretty hard to argue the facts....
Mike isn't the one designing airplanes the last 40 plus years, yet no one has made a production plane with a non conventional tail over that time period. Seems that all those thousands of engineers at however many aircraft manufactures use the same math he does and come up with the same answers....

If the V tail was more efficient, Beech would still be making it and so would everyone else.

"Doctor Killer"

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 17:21 
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Username Protected wrote:
Pretty hard to argue the facts....
Mike isn't the one designing airplanes the last 40 plus years, yet no one has made a production plane with a non conventional tail over that time period. Seems that all those thousands of engineers at however many aircraft manufactures use the same math he does and come up with the same answers....

If the V tail was more efficient, Beech would still be making it and so would everyone else.

"Doctor Killer"


People get over the "emotion" after time passes and logic, reason, common sense and facts come back into view. I agree the V-Tail and MU-2 and some other planes developed a bad wrap, but over time the V Tail has become one of the most beloved planes of all time. Beech could sell them today new IF there was any advantage, but there isn't so they don't build them. When they were introduced in 1947, Beech wanted a plane that was different and the novelty of it sold, not an aerodynamic advantage.

The MU-2 is another perfect example. Market decided they are not worth anything because they were dangerous. Turns out since mandatory training in the plane was required its the safest twin TP. As a result, look at the market slowly increasing.

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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 17:54 
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Username Protected wrote:
Unfortunately, the laws of physics are not determined by a vote.

One has to ask why Beech made EVERY airplane after the 35 less efficient by using a conventional tail.


How do laws of physics explain why a V35B is 3-4 kts faster than identical F33A?


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 Post subject: Re: Cirrus SF50
PostPosted: 07 Jan 2015, 20:27 
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Even though it has similar/more wetted area, it's the one surface less interference drag that makes the Vs faster.

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