Author Topic: 190A5 vs 190A8  (Read 65235 times)

Offline Stoney

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Re: 190A5 vs 190A8
« Reply #300 on: April 16, 2010, 12:47:09 AM »
we got any real world data on turn rate over speed range? and radius over speed range?

so we can look at the relationship, i'm not all in on gaston's point, but it could easily make sense that a pilot could see an decrease in radius without much of a decrease in rate as a "better turning" state for an aircraft and therefore prefer a slower turn speed ...





If the pilot could decrease the radius, he wasn't flying at the best sustained turn rate or radius to begin with.  Best sustained turn rate only occurs at one condition for any single aircraft weight.  Any faster and the radius is larger, any slower and the radius cannot be sustained.  That's why we're being so obstinate here Thor--we're talking about something that is black and white.
"Can we be incorrect at times, absolutely, but I do believe 15 years of experience does deserve a little more credence and respect than you have given from your very first post."

HiTech

Offline stephen

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Re: 190A5 vs 190A8
« Reply #301 on: April 16, 2010, 04:00:48 AM »
And for some reason it took 21 pages to finaly end all the debate?...lol, sounds like an ego trip to me.

Somwhere there is a dead horse being flogged...
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Offline PJ_Godzilla

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Re: 190A5 vs 190A8
« Reply #302 on: April 16, 2010, 04:23:20 AM »
And for some reason it took 21 pages to finaly end all the debate?...lol, sounds like an ego trip to me.
Somwhere there is a dead horse being flogged...

It's like that. Back when I used to work in vehicle dynamics, we used to do something called R202 training. It went something like this:

Customer: I don't like the way this car handles.
Engineer: can you be more specific?
Customer: It's the way this steering wheel is.
Engineer: can you be more specific?
Customer: Look at what happens when I turn it.
Engineer: Can you be more specific?
Customer: At first, nothing....
Engineer... etc.

And what you end up finding out is that the deadband is too large, the gain off-center is too small, and that the efforts just off-center are too small to provide any good on-center feel. In short, the steering is crap for specific reasons but the customer claims the "handling" sucks for general reasons.

Then there's some guy out of left field like you who mocks the effort.

Some say revenge is a dish best served cold. I say it's usually best served hot, chunky, and foaming. Eventually, you will all die in my vengeance vomit firestorm.

Offline FLS

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Re: 190A5 vs 190A8
« Reply #303 on: April 16, 2010, 06:54:38 AM »
It's like that. Back when I used to work in vehicle dynamics, we used to do something called R202 training. It went something like this:

Customer: I don't like the way this car handles.
Engineer: can you be more specific?
Customer: It's the way this steering wheel is.
Engineer: can you be more specific?
Customer: Look at what happens when I turn it.
Engineer: Can you be more specific?
Customer: At first, nothing....
Engineer... etc.

And what you end up finding out is that the deadband is too large, the gain off-center is too small, and that the efforts just off-center are too small to provide any good on-center feel. In short, the steering is crap for specific reasons but the customer claims the "handling" sucks for general reasons.

Then there's some guy out of left field like you who mocks the effort.



That would be a good example if there was something wrong with the FW190 flight model.

Offline PJ_Godzilla

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Re: 190A5 vs 190A8
« Reply #304 on: April 16, 2010, 07:11:48 AM »
That would be a good example if there was something wrong with the FW190 flight model.

It wasn't intended to be about the FM, it was intended to represent the interaction with Gaston. It turns out that his gripe about the FM is a good deal more specific than "the F-dub isn't modelled correctly". In that sense the analogy holds up. It breaks down in the specific case you cite, but that was collateral to my point - that being, often repeated questions, a "drilling down" if you like, is necessary to get at the crux of the issue. Recall, please, that this was in response to the "why 21 pages?" question.

Yes, as far as I can see, the only thing wrong with the f-dub is the minor weight issue cited before.

If you like, I could change my analogy so that the customer is asking for more deadband and less gain but. like I say, the concretes of the example were incidental to the point of R202 - which is translating the non-technical to something specific. Indeed, you could say the Ford and AH briefs are totally different. We seek to give the customer what they want, HTC seeks to give the customer what it wants qualified by and to some extent, only so long as it aligns with FM and historical integrity - two very different missions.

Some say revenge is a dish best served cold. I say it's usually best served hot, chunky, and foaming. Eventually, you will all die in my vengeance vomit firestorm.

Offline FLS

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Re: 190A5 vs 190A8
« Reply #305 on: April 16, 2010, 07:31:33 AM »
... Since that displaces off of hub only slightly, Gaston's power-on pitch moment difference disappears with it.

Yet, my suspicion is, he'll continue to cling to this argument...


Apparently you agree with Steven as well as the point I made.  :aok

The nice thing about these threads is that they're informative as well as entertaining.

Offline Angus

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Re: 190A5 vs 190A8
« Reply #306 on: April 16, 2010, 09:08:41 AM »
Gaston, - LOL, read the word SUSTAINED. SUSTAINED, SUSTAINED, SUSTAINED!!!!
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 hitech

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Re: 190A5 vs 190A8
« Reply #307 on: April 16, 2010, 09:32:45 AM »
we got any real world data on turn rate over speed range? and radius over speed range?

so we can look at the relationship, i'm not all in on gaston's point, but it could easily make sense that a pilot could see an decrease in radius without much of a decrease in rate as a "better turning" state for an aircraft and therefore prefer a slower turn speed ...

Thor going faster will decrease your level turn radius until you reach corner speed. Hence the definition of corner speed, the slowest speed at which you can pull maximum G's. The reason the turn radius decreases is because 2 equations fall out the same, your lift generated (force that makes the turn) and the "Centripetal force" both vary with the square of speed for a given radius. So if you would be doing a loop (with no gravity), you would continue to make the same circle (same radius) as long as you held the same AOA, no mater how fast you would go.

Now when you make a level turn you also need to provide 1g up force  along the the g's of the turn. So at stall speed where you can only produce 1g, you can not turn. but as you go faster the extra G you create all go to turn. So to make is really simple if you are flying at 6 g speed 5g's now go to turn vs 1g for gravity. This makes your circle smaller as you go faster , and hence why corner speed is the best speed to be for best instantaneous turn performance.

Now sustained turn does the exact same thing. The faster you can go at MAX AOA will make both the smallest diameter and the best degrees per sec. So for Gastons logic to be correct.  YOu have to go slower to turn better. This just is not the case at any speed below corner speed which in AH is defined at 6'gs because of black out. So do you know of many planes that can do a continuous 6 g's with out loosing alt?

Now gaston also complete confuses forces and torques. Because (I have not really looked at the net torque because it is not relative)  Torque on the airframe does not make it turn (i.e. change it's vel vector) . it only makes it spin around a point but in no way helps it change direction. This is basic Physics 101 definitions.

So for what gaston claims to be true you would increase speed by decreasing throttle,does that make any since to you?

Now lets look at some of the sustained turn rates he quotes of 250 - 300. These are just insane.

Basic lift equations are the potential lift increase with the square of the speed. So if your 1 g stall speed is 104 (fw ranges) at 208 you could pull 4 gs I do not believe any plane in the game not a plane in the game can do a 4 g sustained turn.

And hence why I said.

Repeat after me. Sustained turn rate decrease with less throttle.

Because the stuff is just simple physics 101. And the stuff grafton spews on the mater is like arguing that an apple will not fall if you drop it.

HiTech

Offline thorsim

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Re: 190A5 vs 190A8
« Reply #308 on: April 16, 2010, 09:36:57 AM »
If the pilot could decrease the radius, he wasn't flying at the best sustained turn rate or radius to begin with.  Best sustained turn rate only occurs at one condition for any single aircraft weight.  Any faster and the radius is larger, any slower and the radius cannot be sustained.  That's why we're being so obstinate here Thor--we're talking about something that is black and white.

that is kinda weird as you guys have always separated the two, rate and radius, and as far as i can tell always admitted that one was achieves at a much slower speed than the other.

however no one here has made any effort to address my question, did you understand it?

i mean if these things are soo absolute then surely there is some pertinent real world data that proves the math.

that is all i asked for, some corresponding real world data, and so far after the several requests i have seen none.

that is disappointing since even gaston has provided at least a fair amount of anecdotal evanesce for his views.

see the problem is that you guys insist on the numbers you produce justify the situation in the game and i and many others have repeatedly on many specific topics have shown that the situation in the game is in direct conflict with real world testing.  something is wrong or something is being missed and that is obvious to many.
i just want to help figure that out.
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Offline thorsim

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Re: 190A5 vs 190A8
« Reply #309 on: April 16, 2010, 09:56:18 AM »
Thor going faster will decrease your level turn radius until you reach corner speed. Hence the definition of corner speed, the slowest speed at which you can pull maximum G's. The reason the turn radius decreases is because 2 equations fall out the same, your lift generated (force that makes the turn) and the "Centripetal force" both vary with the square of speed for a given radius. So if you would be doing a loop (with no gravity), you would continue to make the same circle (same radius) as long as you held the same AOA, no mater how fast you would go.

Now when you make a level turn you also need to provide 1g up force  along the the g's of the turn. So at stall speed where you can only produce 1g, you can not turn. but as you go faster the extra G you create all go to turn. So to make is really simple if you are flying at 6 g speed 5g's now go to turn vs 1g for gravity. This makes your circle smaller as you go faster , and hence why corner speed is the best speed to be for best instantaneous turn performance.

Now sustained turn does the exact same thing. The faster you can go at MAX AOA will make both the smallest diameter and the best degrees per sec. So for Gastons logic to be correct.  YOu have to go slower to turn better. This just is not the case at any speed below corner speed which in AH is defined at 6'gs because of black out. So do you know of many planes that can do a continuous 6 g's with out loosing alt?

Now gaston also complete confuses forces and torques. Because (I have not really looked at the net torque because it is not relative)  Torque on the airframe does not make it turn (i.e. change it's vel vector) . it only makes it spin around a point but in no way helps it change direction. This is basic Physics 101 definitions.

So for what gaston claims to be true you would increase speed by decreasing throttle,does that make any since to you?

Now lets look at some of the sustained turn rates he quotes of 250 - 300. These are just insane.

Basic lift equations are the potential lift increase with the square of the speed. So if your 1 g stall speed is 104 (fw ranges) at 208 you could pull 4 gs I do not believe any plane in the game not a plane in the game can do a 4 g sustained turn.

And hence why I said.

Repeat after me. Sustained turn rate decrease with less throttle.

Because the stuff is just simple physics 101. And the stuff grafton spews on the mater is like arguing that an apple will not fall if you drop it.

HiTech

well then i would submit that since gaston has produced pilot opinions to support his statements that maybe what is happening, since this is all relative ...
(in the sense that your point of comparison and probable point of reference is another aircraft)
then i submit that if it is impossible that the turn rate radius is as he has presented, then maybe it is possible gaston's example of 250-300 is where the 190 had the best relative or comparative turn rate VS. the opponents that pilot had experienced in combat.

i think that that is why many pilots state earlier models but not the earliest models of many aircraft as their favorites even though the performance is clearly improved throughout the type.  i.e. at some point in it's development it had a better relative performance vs. it's opponents that that particular variant faced then the type did during the rest of the pilots time in the type.

you see i don't like the whole "idiot, F.O.S., liar" accusations.  especially since he is relaying the experiences of people with real world experience in these aircraft.  i.e. you may be able to dismiss gaston's conclusions, however his historic references should at least peak some interest if at least just to figure out why they possibly do not seem to jive with the game's representation of the A/C in question.  

BTW thanks hitech that was a clear and helpful post.

+S+

t
« Last Edit: April 16, 2010, 12:47:50 PM by thorsim »
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Offline hitech

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Re: 190A5 vs 190A8
« Reply #310 on: April 16, 2010, 10:01:57 AM »
Thor, It is so bloody simple  its is if you are telling me to go out and drop an apple to prove the real world case, take any plane in the world, and the same things are true. Every plane in the game, every plane that flys (until thrust vectoring) uses the exact same principles. Ive done it in my plane and sure enough it did the exact same as I stated above. Ive done it in cessnas, read Bob Shaws book all state the identical thing.

HiTech

Never mind thor was written before you previous post.
« Last Edit: April 16, 2010, 10:04:52 AM by hitech »

Offline thorsim

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Re: 190A5 vs 190A8
« Reply #311 on: April 16, 2010, 10:10:44 AM »

Never mind thor was written before you previous post.


it's ok i did the same on the previous exchange ...

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Offline Badboy

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Re: 190A5 vs 190A8
« Reply #312 on: April 16, 2010, 03:35:53 PM »
especially since he is relaying the experiences of people with real world experience in these aircraft.  i.e. you may be able to dismiss gaston's conclusions, however his historic references should at least peak some interest if at least just to figure out why they possibly do not seem to jive with the game's representation of the A/C in question.

Firstly, I don't want to labor the obvious, basic and persistant errors in posts that so many others have already corrected, but I would like to say something about the interesting historical references that have been used to support flawed conclusions about sustained turns.

A quick review of some of the anecdotal evidence can reveal how mistakes may have been made.

For example, the combat report by Hanseman, describes how the 109 stopped cutting him off as he cut throttle, and this can be perfectly consistent with aerodynamics and the flight model in AH, but only under certain conditions. For example, Hanseman does not say anything about his initial speed, and if he was above corner velocity reducing throttle would have allowed him to increase his turn rate and reduce his turn radius more quickly. Once he employed flaps, his turn radius would have reduced even further. Nothing was said that is not entirely consistent with real world physics, and Aces High. The mistake would be to make the assumption that Hanseman continued the fight with reduced throttle, and that was somehow responsible for his continued ability to out turn the 109. There is a circumstance where even that is conceivable, and that might be if the aircraft were in a descending low G spiral turn, but Hanseman describes this engagement as occurring at 500ft so that is not the case, because there wasn't room. So, under the conditions described, the assumption that fight was continued with reduced  throttle and that this improved the turn, is clearly false because it is in conflict with basic aerodynamic principles. A much more reasonable assumption would be that once Hanseman had reduced his airspeed below corner, and employed flaps, he would have then increased power as necessary to achieve the best sustained turn.

Another example from the article by Johnson where he describes being out turned by a 190 and where the poster states:

Quote
FW-190A beating in sustained low altitude flat turns a Spitfire Mk V that is running at "wide-open throttle", WITH post-war hindsight:

However, if you read Johnson's article it presents a very different picture of what really happened, that is also perfectly consistent with aerodynamics. Firstly, when Johnson describes turning hard to the left and whirling around on opposite sides of what seemed to be an ever decreasing circle, he gave no indication or details of that phase of the fight, other than to say they were on opposite sides of the circle, which indicates that during that time the fight may have remained neutral. With no indication of how long that phase lasted, we can only speculate, but it is possible that if both aircraft were at high speed, and they both pulled the same G, they would have been able to match each others turns for a time while their speeds were decreasing. However, where Johnson initially describes being out turned by the 190 they were not at low altitude, and they were not in flat turns, as indicated in the quote above. They were high enough that Johnson was able to enter a near vertical dive after he conceding the fight, and the turn was not flat, Johnson actually said he was in the "tightest of vertical turns" and that he was at full throttle and greying out. What difference does that make?  Firstly, you would expect the 190 to be superior in the vertical so no real surprise there, but he also describes being at full throttle and greying out, which indicates that at that time the fight was occurring at the relatively high speeds and load factors. Bearing in mind that two aircraft at the same speed and load factor will turn at exactly the same rate and radius, this fight may have been determined partly by the superiority of the 190 in the vertical, and possibly by differences in the G tolerance of the pilots. After all, for all we know, Johnson may have had a bad night and been greying out at relatively low G, while the German stud flying the 190 was able to pull harder, generating the rate and radius necessary to give Johnson the scare he needed to beak off into a near vertical dive. When Johnson says "My over-confidence of a few seconds before had already given way to irritation at losing my opponent" he gives us the clue that this phase of the fight was infact brief, and that his perception of being out turned was arrived at quickly, and not after sustained turning. Once he had broken off into a dive the 190 was in trail and in the control position, any further turning by Johnson appears to have only been used to align himself with the Ships.

I would say that this combat report says a lot more about the survival instincts and perception of a great Ace, than it does about the performance of the aircraft involved. It is also possible to see from both reports that anecdotal evidence, typically sparse in fundamental detail and lacking any basic technical facts, or information about the condition or configuration of the aircraft involved, can very easily be misinterpreted.

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Offline thorsim

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Re: 190A5 vs 190A8
« Reply #313 on: April 16, 2010, 03:57:43 PM »
yes but we also have testing that disputes the stall behavior of the 190, have been unable to produce operator air-force supporting evidence for the extent of it's twitchy behavior in higher g, have had a 4g limit in game that has yet to be supported, have rooted out a roll tendency in the game for the 109(at least the F) that is also unsupported in any testing yet shown.  we have a better general understanding of the excellent real world handling qualities of the 190s, and a definitive weight disparity in some of the 190 FMs in the game.  

IMO this has been a worthwhile discussion, and in my experience discussions such as this one can lead to excellent FMs that both reflect the definable mathematics/physics, and the historic testing and literature.  

i am all for explaining pilot observations with known aerodynamics of the aircraft, i think that usually the one tends to support the other.  where there are discrepancies however they imo should be used as an opportunity to either support the game representation, or to better understand the aircraft being "recreated" and possibly re-evaluate some things in the game/s. or at least ad them to the wish list...


 
« Last Edit: April 16, 2010, 06:15:12 PM by thorsim »
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Offline Badboy

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Re: 190A5 vs 190A8
« Reply #314 on: April 16, 2010, 07:19:20 PM »
thorsim,

in my experience discussions such as this one can lead to excellent FMs that both reflect the definable mathematics/physics, and the historic testing and literature.

Probably not in this case, because when I read this thread the things that stand out the most are the degree of misunderstanding of basic physics, the misinterpretation of anecdotal evidence and technical reports, and the abysmal polemics in terms of both integrity and logic. Much of it appears to be in support of or in contention with some feature or other of someones favorite aircraft, and frankly, I've seen more coherent reasoning among squabling six year olds.

As an example of how easily misunderstanding can arise:

have had a 4g limit in game that has yet to be supported

There simply isn't "a 4g limit in game". Assuming you are referring to the 109s or 190s I just checked them all and have no difficulty reaching 9G. I suspect, you probably meant to refer to something else, such as the control force modelling at high speed perhaps? Regardless of the merits of modelling control forces, or whatever you actually meant, you may appreciate how easy it is for misunderstandings to arise when people use the wrong terms or use well defined terms incorrectly, particularly when that degree of confusion proliferates the usual ill conceived petition for change that I've seen here. Not least of all when in previous responses it has been shown that various sources are being construed in support of arguments that defy the laws of physics.



Badboy
« Last Edit: April 16, 2010, 07:34:29 PM by Badboy »
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