Author Topic: Max CL and its effect on performance  (Read 2473 times)

Offline Angus

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Max CL and its effect on performance
« Reply #60 on: October 18, 2004, 04:08:18 PM »
Scratching my head here:confused:

Ok, so Willy modded the original Handly Page mechanism so that the slats would deploy relevantly to stall condition at any speed, not just the slow speeds. Am I understanding right?
So, they still worked at slow speeds right, just no particular upper limit?

So,providing I understand you correctly, it comes to this:
"Don't try to deceive yourself, Angus. The Me 262, F-86 and F-4 are no slow "bushplanes", but a hell of a lot faster than the Me 109, and Handley-Page slats worked great for them. "

So you're saying that both the F86 and the F4 had the Messerchmitt mod rather than the original?

Eager to learn, always, and not immune to mistakes, so sorry if I misunderstand.:o
It was very interesting to carry out the flight trials at Rechlin with the Spitfire and the Hurricane. Both types are very simple to fly compared to our aircraft, and childishly easy to take-off and land. (Werner Mölders)

Offline Meyer

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Max CL and its effect on performance
« Reply #61 on: October 18, 2004, 04:24:14 PM »
AFAIK the slats open at a certain AOA, regardless the speed.

A couple of interesting links about the subject :)

http://109lair.hobbyvista.com/techref/systems/control/slats/slats.htm

http://simhq.com/_air/air_002b.html

Offline HoHun

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Max CL and its effect on performance
« Reply #62 on: October 18, 2004, 04:38:52 PM »
Hi Angus,

>Scratching my head here:confused:

Sorry, I guess that's my fault! I'll try to be more accurate now :-)

>Ok, so Willy modded the original Handly Page mechanism so that the slats would deploy relevantly to stall condition at any speed, not just the slow speeds. Am I understanding right?

The original mechanism were free-moving slats. The initial Me 109 design had an additional locking mechanism that did not allow the slats to come out of the wing unless 10° or more of flaps were deployed. This had nothing to do with the flap design, but it was old-fashioned mechanics.

(As I read about the SM79 having a similar mechanism, that might have been common practice then.)

In 1936, Messerschmitt considered the option of leaving the slats free throughout the entire flight envelope. That was apparently not common practice, at least not for high-performance planes, as intensive research was required. Gustav Lachmann of Handley-Page's contributed, obviously tackling the problem of high speed flight for the first time, too.

(Lachmann suggested a pneumatic emergency retraction for the slats in case they should induce an irrecoverable spin. Only during the trials it became clear that they actually made spins less likely and helped with recovery.)

>So, they still worked at slow speeds right, just no particular upper limit?

No, just no mechanical downlock anymore. The slats are not triggered by speed, even though it's often presented that way in books and on the internet. They are triggered by the airstream dependend on angle-of-attack (you could also say dependend on lift coefficient, because AOA and Cl are connected), so they'll come out at high speed in a high-G turn just the same as at slow speed in 1 G flight.

>So you're saying that both the F86 and the F4 had the Messerchmitt mod rather than the original?

Well, Messerschmitt didn't actually change the slats, he merely was the first (as it looks) to use them on a high-speed aircraft. As far as I know, the F-86 and the F-4 had the same type of slat as the Me 109, which basically was what Lachmann invented at Handley-Page in 1919.

>Eager to learn, always, and not immune to mistakes, so sorry if I misunderstand.:o

Probably I mis-explained :-) Sorry for that!

Regards,

Henning (HoHun)

Offline Charge

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Max CL and its effect on performance
« Reply #63 on: October 19, 2004, 02:28:18 AM »
FYI, the first F4s did not have the slats and in Vietnam skies it was evident that F4 could not rely entirely on its missiles but had to "mix it" with enemy fighters. Violent high speed maneuvers tended to cause "departures" which were not always recoverable so computer controlled slats were installed. The top speed dropped though, but the effect on handling was considered so big that it became a default configuration in F4.

-C+
« Last Edit: October 19, 2004, 02:35:19 AM by Charge »
"When you wish upon a falling star, your dreams can come true. Unless it's really a giant meteor hurtling to the earth which will destroy all life. Then you're pretty much screwed no matter what you wish for. Unless of course, it's death by meteorite."

Offline Angus

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Max CL and its effect on performance
« Reply #64 on: October 19, 2004, 05:33:39 AM »
Ok.
So what Willy did was to remove the flap-related mechanism (lock) and allow again the free movement of the slats.

My friend is on the hunt for Rall's slat quote, - he has it on video tape. I'll post it as soon as I get it.

Regards.
Angus
It was very interesting to carry out the flight trials at Rechlin with the Spitfire and the Hurricane. Both types are very simple to fly compared to our aircraft, and childishly easy to take-off and land. (Werner Mölders)