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Old October 22nd, 2007, 17:05   #1
ppragman
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Default Be-1900 Airfoil and mach tuck...

So, I know this guy who is absolutely afraid of the barber poll in the 1900. He doesn't want to nose over to the poll whenever he starts his descent, and is terrified that he will nose over and enter a "mach tuck." This is rediculous, but there is no way for me to prove it unless I can get some info on the airfoil of the 1900. If I could find out what the critical mach number is I could prove to him that at .48M (Mmo in the 1900c) we are nowhere near the critical mach #. Anyone know where to look?
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Old October 22nd, 2007, 18:03   #2
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Default Re: Be-1900 Airfoil and mach tuck...

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there is no way for me to prove it unless I can get some info on the airfoil of the 1900. If I could find out what the critical mach number is I could prove to him that at .48M (Mmo in the 1900c) we are nowhere near the critical mach #. Anyone know where to look?
The Beech 1900 (C-12) uses the NACA 23018 for the root and the NACA 23012 for the tip. NACA often uses these airfoils for a variety of tests, so you might be able to get the figure from one of their reports (Will take a lot of work.) I have a book at home which might have the data.

.48M would be a very low critical mach, as you know.
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Old October 22nd, 2007, 19:39   #3
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Default Re: Be-1900 Airfoil and mach tuck...

Your answer won't lie in the horizontal airfoil (the wing) but in the vertical ones (the props). A turboprop is mostly limited to such a low mach to prevent the propellers from going supersonic (specifically the tips). Mach tuck won't be an issue.

On a lot of the racing airplanes you will see shortened diameter propellers that enable the airplane to go faster without losing efficiency to mach effects at the prop tips.
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Old October 22nd, 2007, 19:40   #4
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Default Re: Be-1900 Airfoil and mach tuck...

thanks a lot
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Old October 22nd, 2007, 19:42   #5
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Default Re: Be-1900 Airfoil and mach tuck...

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Originally Posted by B767Driver View Post
Your answer won't lie in the horizontal airfoil (the wing) but in the vertical ones (the props). A turboprop is mostly limited to such a low mach to prevent the propellers from going supersonic (specifically the tips). Mach tuck won't be an issue.

On a lot of the racing airplanes you will see shortened diameter propellers that enable the airplane to go faster without losing efficiency to mach effects at the prop tips.
That's pretty useful info. I think it's rediculous worry, but that's why I'm trying to get this info to prove it to him.
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Old October 22nd, 2007, 20:53   #6
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Default Re: Be-1900 Airfoil and mach tuck...

If it goes any faster all of those ridiculous winglets and vortilons and whatever the heck else those things the engineers stuck on that airplane to make it fly are called might fall off!
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Old October 22nd, 2007, 21:41   #7
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Default Re: Be-1900 Airfoil and mach tuck...

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If it goes any faster all of those ridiculous winglets and vortilons and whatever the heck else those things the engineers stuck on that airplane to make it fly are called might fall off!
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Old October 23rd, 2007, 08:41   #8
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Default Re: Be-1900 Airfoil and mach tuck...

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So, I know this guy who is absolutely afraid of the barber poll in the 1900. He doesn't want to nose over to the poll whenever he starts his descent, and is terrified that he will nose over and enter a "mach tuck." This is rediculous, but there is no way for me to prove it unless I can get some info on the airfoil of the 1900. If I could find out what the critical mach number is I could prove to him that at .48M (Mmo in the 1900c) we are nowhere near the critical mach #. Anyone know where to look?

I've been flying the 1900 for about six months.. had a guy set off the overspeed for a second once.

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Old October 23rd, 2007, 09:28   #9
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Default Re: Be-1900 Airfoil and mach tuck...

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...terrified that he will nose over and enter a "mach tuck." This is ridiculous, but there is no way for me to prove it unless I can get some info on the airfoil of the 1900.
Technical aspects aside, if it were "theoretically" possible for a 1900 to enter mach tuck, doesn't he understand that certification margins would preclude him from exceeding such a speed under normal operations?

B1900D
Mmo .48
Max Alt FL250

King Air 300/350
Mmo .58
Max Alt FL350

http://rgl.faa.gov/Regulatory_and_Gu...FILE/a24ce.pdf


Please tell me he isn't a PIC......
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Old October 23rd, 2007, 11:06   #10
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Default Re: Be-1900 Airfoil and mach tuck...

ROFL Some one told him the barber pole was the limit for mach tuck??!!? For your airplane to be able to mach tuck, it needs to not be built like a dump truck!
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Old October 23rd, 2007, 12:58   #11
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Default Re: Be-1900 Airfoil and mach tuck...

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Please tell me he isn't a PIC......
No, thank god, he's one of the other FOs
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Old October 23rd, 2007, 12:58   #12
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Default Re: Be-1900 Airfoil and mach tuck...

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ROFL
that's what I said
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Old October 25th, 2007, 13:49   #13
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Default Re: Be-1900 Airfoil and mach tuck...

Ride the pole like a stripper! Especially on the last leg or min day.
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Old October 26th, 2007, 10:44   #14
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Default Re: Be-1900 Airfoil and mach tuck...

Mach tuck in a Beech........Not gonna happen. Period.

The speed limitations like were said earlier are to prevent the props from going supersonic. Its the same reason helicopters don't go that fast.
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Old October 26th, 2007, 18:24   #15
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Default Re: Be-1900 Airfoil and mach tuck...

I know, that's what I said
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Old October 26th, 2007, 22:14   #16
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Default Re: Be-1900 Airfoil and mach tuck...

I would ask him how it is that mach tuck could be a risk on a plane that doesn't even go half the speed of sound (.48). Shouldn't it be obvious to an airline pilot that no local flow over any surface of an airplane that goes so slow will get anywhere near supersonic? (Prop tips excepted.)

Ask him to define Mmo.
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Old October 27th, 2007, 01:23   #17
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Default Re: Be-1900 Airfoil and mach tuck...

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on a plane that doesn't even go half the speed of sound (.48)
Actually, for airfoils that weren't intended for high speed, critical mach can be quite low. I'm looking at some data indicating .58 or so for an airfoil similar to the one on the Beech, and that's at a low AOA. Put this aircraft into a 60 degree bank and the critical mach would be much lower.
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Old October 27th, 2007, 02:48   #18
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Default Re: Be-1900 Airfoil and mach tuck...

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Actually, for airfoils that weren't intended for high speed, critical mach can be quite low. I'm looking at some data indicating .58 or so for an airfoil similar to the one on the Beech, and that's at a low AOA. Put this aircraft into a 60 degree bank and the critical mach would be much lower.
Put anything into a 60 degree bank and the critical mach should be lower. Let's just say then that hypothetically, the Mcrit on the 1900 is .58, a full 10% higher than .48. So let's say that you roll it over into a 60 degree bank, if you maintain altitude, then there's no way you'll even be at the barber poll. If you roll over into a 60 degree bank while diving then you might have some issues assuming Mcrit is lowered more than negligibly, but how often are you going to roll into a 60 degree bank in a dive? I'm a freight dog and that's rediculous, we don't even do that to get into dutch harbor.
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Old November 8th, 2007, 16:00   #19
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Default Re: Be-1900 Airfoil and mach tuck...

I'm surprised no one here asked if this guy went to GIA ???

Did he ??
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