Author Topic: The "Curious George" or a "Castrated George" ?  (Read 585 times)

Offline Vermillion

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The "Curious George" or a "Castrated George" ?
« on: November 29, 1999, 05:48:00 PM »
I know this is long but please stick with me and consider my points

Ever since I first heard of Aces High, and started visiting this BBS, I was excited. When Pyro announced that he would be doing either a Ki84 or a N1K2 as the initial Japanese fighter, I was ecstatic, since the N1K2 was my favorite plane in AW and I had always wanted to see one done in WB's.

Now back in AW, we called the N1K2 "George" the "Curious George" because it was an aircraft with unique qualities.  It was fast below 15k feet (second in PAC only to P-51), had excellent acceleration, excellent guns, and was second in climbrate to only the Spitfire (PAC). It also had its drawbacks, it has poor roll rate, it has poor high speed handling,  a "middle of the pack" turning ability that really bled E badly, and its power dropped off rapidly above 15k.

I expected to see something similar in AH. Yes Flightmodels and Physicmodels may differ, but in each game (AW, AH, WB, and even FA) the planes compared the same.  A P-38 is a P-38. The Fw190 is the Fw190. A P-51 matches up to a Me-109 the same in all games.

The Aces High  N1K2 is the first to break that mold.

When the N1K2 first appeared in AH, I felt that it was performing poorly, so I did some testing. That testing showed that it is 25%-30% too slow at all altitudes, and that its climbrate is 25%-30% too low at all altitudes, when compared to the data used in AW for the same plane.  These can be found in two N1K2 Flight Testing threads in this forum, along with the TAIC data I am refering too.

But Pyro sure got the "poor" qualities down exactly  

Pyro confirmed that the data I used to compare against was historical data from an Army TAIC Unit, but he felt that he wasn't convinced that the data was representative, and he based the N1K2 flight model upon other data.

So I started looking for this "other" data, or any other attribute that I could find, that would indicate the George performed the way it does in AH.  The USAF museum says the data doesn't exist, and the USN Aviation Musuem hasn't responded to my inquires yet.

So I started to look at what is called "Engineering Indicators". These are factors that can be derived from more common data that indicate the general performance of an aircraft, or used to compare a relative performance between different aircraft types.  Admittedly these are not enough to construct a flightmodel, but they should be sufficent to indicate if a set of data (the Army TAIC data in this case) is in the ballpark.

So I contend that the N1K2 is too slow, and that its climbrate & acceleration (two closely related attributes) are too low. So what indicators can I use for these?

TOP SPEED
AHT and other engineering texts, indicate that the best way to compare "theoretical" top speeds is too look at the ratio of Horsepower(hp) to Zero Lift drag (f). Zero Lift Drag is the primary drag component at higher speeds, and horsepower is a general indicator of thrust (if prop efficencies were available an actual thrust to drag ratio could be computed).

Now, using AHT, I calculated the above ratio at Sea Level for the P-51, the F4U-1D, and the Me-109G10. Critical data (Cd) for the other fighters in AH were not available for these calculations, so they are not shown here. I also calculated it for the P-47D and the F6F-3, since they were aircraft of the same general size/horsepower category of the N1K2 and were useful in this comparison. One critical piece of information, the zero lift drag coefficent (Cd), is however not available for the N1K2. So what I did was calculate it with 3 seperate values. The worst possible drag coefficent I have seen ( F2A Brewster Buffalo ), a middle of the road coefficent for a radial ( F4U-1D ), and the best coefficent for a radial fighter ( P-47D ).  I highly doubt that the N1K2's drag coefficent is as bad as the Buffalo's, but I have included it here as a "worst case" scenario.

   

Lets look at the results. As you can see the "indicator" is almost dead on in ranking the flight test performance of  the aircraft.  The only anomaly is the Me-109G being faster than the P-51 by a very small amount, and this can be attributed to differences in Propellor efficencies.

If you look at the results for the N1K2 you can see that the *3 case data (P-47D drag coefficent) is probably incorrect since it would indicate that it would be faster than the P-51, something the historical TAIC data did not indicate. However if you look at either the "middle of the road" the *2 case (F4U-1 drag coefficent), or even the worst case *1 data ( F2A Buffalo drag coefficent), you will see that they BOTH support the TAIC data in that the N1K2 should be faster at sea level than the F4U-1.  In Aces High, the N1K2 is the slowest plane in the game, well below planes that are slower than the F4U-1.

Conclusion: HP/ Zero Lift Drag Ratio's  heavily support the TAIC data over the current modeling.

CLIMB & ACCELERATION
Climbrate and Acceleration are two factors that are directly related, and are proportional to one another.  If you have high climb rate you have high acceleration.

The best "indicator" of climbrate and acceleration, is typically considered to be powerloading.  Powerloading is simply the weight of theaircraft, or loading, divided by the power, or horsepower.

One way to do this is too compare at the fully loaded "take-off" weight.

   

The results again show that this "indicator" corresponds very well with flight test data. The La5 and Me109 are almost identical in the top spot, with the Spitifire in second, and the rest line up from there exactly as we see them in the game.

As can be seen, this "indicator" data matches the TAIC data,  in that the N1K2 should be a good climber second only to the Spitfire in late war Pac planes.  In Aces High, the N1K2 has a poor climb rate comparable to or less than the P-51D, which should be one of the slowest climbers.

Conclusion:  Powerloading  heavily support the TAIC data over the current modeling

Powerloading can also be calculated using an "empty" weight.  This is done to remove fuel and other expendables as a factor from the calculation. In other words, if you load each aircraft with the exact same amount of fuel and no ammunition, this is how they would compare.  It is presented here for informative purposes.

   

All this data & calculations adds up to one conclusion for me.

The general data and "indicators" that work for every other aircraft in Aces High (or in reality any aircraft, for that matter), just do not support the current modeling of the N1K2 George.  In fact, they support in every way the historical data I presented (TAIC).

History supports the TAIC data also.  Every description that I can find of the N1K2 uses terms like "... one of the most successful land-based fighter aircraft of the war." or " a truely outstanding fighter, capable of meeting on equal terms the best Allied Fighter Aircraft." There is even one account of where a single N1K2 engaged a group of 12 (yes twelve) F6F Hellcats, destroying four of them and forcing the others to break off combat. And this was a point in the war where the American pilots were vastly more experienced than their Japanese counterparts.  Does this sound like the AH N1K2? Or do you think this could happen like described? I would have to answer both questions with a "not on a cold day in hell"  

I know that somone's first response to this post is gonna be "Well.. I can get kills in it, you just suck".  Well, you may be right   but the issue is the accuracy of the plane model, NOT the individual skills of a pilot.  I also know several of you tend to not like mixing of Euro and Pac aircraft, so you are just down on any Japanese aircraft period.  But consider this, next time it might be YOUR favorite plane that has its flight model  "flawed".

Right now, the Aces High N1K2 is being flown in the arena because it has good guns, is stable (not bouncy), and it has moderate turning ability. But once more real TnB aircraft are modeled  (Zero, Hurri, or F4F for instance) people will begin to realise how mediocre the George is in a turnfight and its use in the arena will fall to almost nothing.  Wasting what was in reality a really effective aircraft, and turning it into another "could have been".

Pyro I know you have stated that in the next revision, you will begin to re-evaluate the flight models, and fine tune them.  Please reconsider the use of the TAIC data.  It seems to me that it is much more "likely" than whatever data we are currently using.

So which are we going to get?

The "Curious George" or a "Castrated George" ?

PS: If you won't reconsider, I guess I am going to have to start campaigning for the P-63 KingCobra,  the Yak-3, or the Ki-84  

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Vermillion
WB's: (verm--), **MOL**, Men of Leisure,
"Real men fly Radials, Nancy Boys fly Spitfires   "

[This message has been edited by Vermillion (edited 11-29-1999).]

Offline wells

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The "Curious George" or a "Castrated George" ?
« Reply #1 on: November 29, 1999, 07:42:00 PM »
I agree Vermillion!

The key being 'How much power did the engine produce?'.  Now, most sources say 1990 hp to 1625 hp @ 20k or so (almost identical output to the R-2800, making direct comparison with the F6f and F4u).  I have seen no other figures of lower value.  

What stands out is the smaller diameter propeller, comparitively speaking.  Having to turn 3000 rpm compared to 2700 could explain that.  However, thrust efficiency will be less as a result.

The drag is closely related to the wing area (being over 1/2 the total surface area and most fuselages look similar).  The characteristics of the George's wing is that of high aspect ratio (over 6:1) meaning lower induced drag and a lower overall area (253 vs 314 for F4u and 334 for F6f).  Speed will vary with the square root of the drag (or wing area ratios) and with the cube root of the prop diameter relationships.

Combining the 2 factors and comparing to the F6f or F4u, I get the following speed relationships...

F4u: (314/253)^1/2 * (3.1/4.0)^1/3 = 1.023
George is 2.3% faster than F4u

F6f: (334/253)^1/2 * (3.1/4.0)^1/3 = 1.055
George is 5.5% faster than F6f

With the F6f being capable of 380 mph with MIL power and the F4u being capable of 395 mph with MIL power (data from AHT), that puts the George in the 401-404 mph range.  Speeds at sea level working out to 347-350mph.


Nath-BDP

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The "Curious George" or a "Castrated George" ?
« Reply #2 on: November 29, 1999, 11:09:00 PM »
Remember, N1K2 didnt have SUPERCHARGERS.

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Offline wells

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The "Curious George" or a "Castrated George" ?
« Reply #3 on: November 30, 1999, 12:07:00 AM »
I found a reference to the Homare 22 engine that was apparently used in a prototype of the 'Sam', but was changed due to very poor altitude performance.  It put out 2000 hp for takeoff, but only 1300 hp @ 6000m.  If this is indicative of the Homare 21 engine used in the George, then 370 mph is reasonable, but sea level speed should still be around 350 mph and initial climb near 4k/min.  I'm still looking for more on these engines!

Offline leonid

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The "Curious George" or a "Castrated George" ?
« Reply #4 on: November 30, 1999, 03:58:00 AM »
Verm,
I can understand your concern especially since the niki is your baby, but here are a couple things you should consider:

1) Not all flight data resides in the USA.  Who's to say that someone in Japan still holds flight data in Japan?  The US military holds no real flight data on Soviet WWII aircraft, and in fact, you need to go to Germany or Russia if you want that.  I do know that when the WB Yak-3 first came out many Russian players were very critical of the FM.  Later on, many of them realized that in fact the WB Yak-3 was a very good simulation of the real one, and some have even said so to Pyro publically.

2) I find the N1K2 a very formidible opponent, and I fly the La-5FN.  It's one weakness appears to be that it is somewhat fragile(only somewhat, mind you), but that,s about it.

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ingame: Raz

Offline Vermillion

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The "Curious George" or a "Castrated George" ?
« Reply #5 on: November 30, 1999, 06:41:00 AM »
Nath: everything that is calculated is at SEALEVEL, where it produces basically the same horsepower as the R-2800 that powers the F4U and F6F (1990hp vs 2000hp). And you are correct the power of the Homare 21, does fall off rapidly over 15k due to its lack of a good supercharger (One of its stated weakness's).  But that doesn't effect its low level performance which is what I am speaking off.

Leonid: It should be an even more formidable opponent   And I hope to someday see some data surface somewhere. But my point is that everything I can find, points to the TAIC data being better than what we have now.

Question for you. If they took a La5 reduced its speed and climbrate, but reduced its wingloading by 30% so that it turned better and added two cannons.

Would that be acceptable to you?

It would still be a "formidable opponent", but then it really wouldn't be a La5 would it?  

Thats the way I feel about the current George. Its not really a "George", its a AH476z-e "Fantasy Freddy", IMO.      

It should fly like a slightly more manueverable late war 109, and right now it flys like a fat zeke.

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Offline leonid

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The "Curious George" or a "Castrated George" ?
« Reply #6 on: November 30, 1999, 09:02:00 AM »
Verm,
You think the niki should turn just slightly better than a late 109?  Wow, I'll check my wing loading figures before addressing that(am at work).  

I have problems with the TAIHC-derived AW data that you have, since it gives extremely weak performance for the Bf 109K-4, which should be a real Beast in speed and climb.  Thus, if that data appears erroneous, then ... ?

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Offline Vermillion

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The "Curious George" or a "Castrated George" ?
« Reply #7 on: November 30, 1999, 10:02:00 AM »
Leonid, Your comparing two different datasets from two different sources.

The AW Data Charts I presented, came from various sources, mostly the NASM, NACA, USAF Museum, and others.  Its a compilation, presented in a single place for comparison purposes.

The data for the N1K2, came from that Army Intelligence unit that Pyro called the TAIC (forget acryonym meaning).

Just because you feel that the Chart Data for the Me-109K was wrong (it very well may be, I don't disagree), that doesn't make the N1K2 data incorrect.  

That would be like saying that since the F4U-4 in Warbirds is 20mph too slow, EVERY flightmodel in Warbirds is wrong, by association.

Everything I can find on the N1K2, points towards performance in the approximate range of the TAIC data.

Thats the point of the post. I am basically challenging everyone out there to provide some hard data that would indicate that the AH N1K2 model is the correct one.

And by hard data I mean either primary flight test data or some other engineering analysis. Not the top speed listed in Janes Fighters of WWII, or any other coffee table reference book.

And its not like we are quibbling over a minor 5 mph IAS difference at 25k alt here.  The difference is an approximate %25 reduction to speed and climb over the entire altitude range. That is a huge difference.

Hey if someone can prove me wrong, I will happily shut up.  

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Offline Vermillion

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The "Curious George" or a "Castrated George" ?
« Reply #8 on: November 30, 1999, 10:18:00 AM »
Oh and information needed to calculate wingloading is available in the above charts (at work myself, so this is quick and dirty)

But it comes out to be

Loaded:  
N1K2 34.99 lbs/sq ft.
Me109G10 43.33 lbs/sq ft.

Empty:
N1K2 23.25 lbs/sq ft.
Me109G10  34.06 lbs/sq ft.

The comparison between the two was more in speed/climb/acceleration.

Yes at lower altitudes, the N1K2 would be much more manueverable than the 109G10, since it has 68% more wing area, and more power (140hp) to offset the increased drag.

However as altitude increased, the power difference would decrease until the 109 horsepower would be greater, and that increased wing area would be a liability causing greater drag, and therefore less thrust and lift.

In short, under 15k feet in a 1v1 I would bet on the N1K2, but get up to the higher altitudes and I would bet on a 109G10.

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Vermillion
WB's: (verm--), **MOL**, Men of Leisure,
"Real men fly Radials, Nancy Boys fly Spitfires ;) "

Offline xela

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The "Curious George" or a "Castrated George" ?
« Reply #9 on: November 30, 1999, 03:03:00 PM »
Maybe its all the armor Pyro put on it, cause it now absorbs quite some punishment  

Offline Pyro

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The "Curious George" or a "Castrated George" ?
« Reply #10 on: November 30, 1999, 08:26:00 PM »
A short rebuttal:  

I looked at your charts again.  TAIC is Technical Air Intelligence Center.  It's written right there on your chart.  That's not an actual document BTW.  At any rate, the George that the TAIC looked at was an N1K1-J, not the N1K2-J.  That would mean that the AH N1K2 should perform even better than that.

I can't answer for how someone else models the planes in their game so it does no good to hold that over my head.  If you're expecting the F4U-1D in AH to climb at 3800 fpm up to 20K like the one in that chart, you'll be in for a surprise there too.

The R2800 planes are given the short end of the stick in the charts in your post since their HP is shown at military and not emergency power.  Similarly, the 51 is shown with 1500 HP in the first chart but 1590 in the second and third charts.  It should be 1720 for max power.

Since the drag coefficient you are using is relative to the wing area, you just can't interchange one with another.  If you take a plane and reduce its wing area, its drag coefficient will be higher than when it had the bigger wing.  Hypothetical example: Take two 100 sf wings and a fuselage.  Individually they each have a flat plate equivilent of 2.  Put them all together and you end up with a Cd of .03.  Now remove half of each wing.  Did your f just drop from 6 to 4 or to 3?  Is your Cd still .03 or is it now .04?

I was looking at your f values from AHT and was curious about them so I made a little spreadsheet.  The F6F and F4U have impossible values.  I didn't check them all but here's an example.  For the F4U to achieve the emergency speed cited in the book at the power level cited and using that f value of 8.38, it would require a propeller efficiency of 123%.  Something doesn't fit there and it's not the power or performance.  Check it out for yourself.  Drag = f / density * .5 * velocity^2.

On the power loading chart, it's biased against the American planes as mentioned earlier, but the empty weights are also misleading.  The reason is that an empty weight figure can mean different things.  It might mean totally empty- no guns, no trapped fluids, nothing; or it might refer to basic weight with pretty much everything except fuel, ammo, and pilot.  This is hard to tell unless you have a breakdown of the weight.  If you don't then you have to make some calculations.  In your chart, it looks like some of the weights are empty while others are basic.  For example, the empty weight of your FW looks to be the basic weight while the P-51 looks close to the real empty weight.  

As for the weight of the N1K2, that's subject to debate as well.  Some say it's 8818 loaded while others say 9040 loaded.  I'm skeptical as to the precision of those numbers as they happen to be exactly 4000kg and 4100 kg respectively.  For empty weights, I've seen 5858 and 6357.  I can't make sense out of the 5858 figure.  It doesn't add up.

Quote:
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History supports the TAIC data also. Every description that I can find of the N1K2 uses terms like "... one of the most successful land-based fighter aircraft of the war." or " a truely outstanding fighter, capable of meeting on equal terms the best Allied Fighter Aircraft." There is even one account of where a single N1K2 engaged a group of 12 (yes twelve) F6F Hellcats, destroying four of them and forcing the others to break off combat. And this was a point in the war where the American pilots were vastly more experienced than their Japanese counterparts. Does this sound like the AH N1K2? Or do you think this could happen like described? I would have to answer both questions with a "not on a cold day in hell"
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It has one of the higher K/Ds in AH so why  not?

You point out the fact that it is widely mentioned as a fine fighter but fail to also point out that it's widely mentioned that it didn't fare so well as an interceptor due to its climb rate and high altitude performance.  This is supported by the fact that the N1K5 was under development to rectify those shortcomings.  Most figures put its time to 6000 meters at 7' 20" or an average rate of under 2700 fpm.  That's 900 fpm less than your climb rate *at* 6000 meters.

You cite the account of Warrant Officer Kaneyoshi Muto which is found in pretty much everything ever written on the George.  Looking to a single event as proof is pretty weak as there can be a lot of extenuating circumstances.  Maybe the other planes were returning from a strafing mission low on fuel and ammo and got in over their heads.  Who knows?  In this case, there are other extenuating circumstances that are now known.  Henry Sakaida debunks this story in his book _Imperial Japanese Navy Aces 1937-45_.  A quote:

"On 16 February 1945 the US Navy launched its first carrier raid against the Tokyo area, and Muto, piloting a new Shiden-Kai ('George') from the evaluation department of his air group, joined his squadronmates in their efforts to thwart the raiders.  Muto became embroiled in a fierce dogfight with F6Fs from VF-82 that saw four Hellcats downed."

"Desperate to find heroes to help deflect news of the seemingly endless series of military defeats, the Japanese press found WO Kaneyoshi Muto's deeds during this sortie ideal for their propaganda purposes.  An exaggerated version of the combat was duly spread that saw Muto single-handedly take on 12 F6Fs, destroying four- this myth survives to this day."

As to the TAIC calculations being off, there's a precedent with the George for that as well.  According to Francillion on the George prototype: "Performance was also disappointing and the aircraft achieved a top speed of only 310 kt (357 mph) whereas its calculated maximum speed had been estimated at 350 kt (403 mph)."  This backs up the widely published speeds in the 360-370 range and not a 400+ figure.

All that said, I do wonder primarily about the low alt speed and will take a look at it again before the beta is through.  The George is a mysterious plane and there's not a lot of info on it.  I'm not afraid to model a plane like this however.  I will do what I think makes the most sense to me and try and cut through those things that don't.  Just imagine what it would be like if our roles were reversed.



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Offline wells

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The "Curious George" or a "Castrated George" ?
« Reply #11 on: November 30, 1999, 10:36:00 PM »
Pyro,

Those drag coefficients are figured for 250 mph at sea level and include the induced drag component, so it's useless to use as a basis for top speed measurements.  Don't you have this book yet?    

 
Quote
Since the drag coefficient you are using is relative to the wing area, you just can't interchange one with another. If you take a plane and reduce its wing area, its drag coefficient will be higher than when it had the bigger wing. Hypothetical example: Take two 100 sf wings and a fuselage. Individually they each have a flat plate equivilent of 2. Put them all together and you end up with a Cd of .03. Now remove half of each wing. Did your f just drop from 6 to 4 or to 3? Is your Cd still .03 or is it now .04?

You are right for this example, but generally speaking, planes with small wings have small fuselages as well, so the 2 pretty much go hand in hand and wing area can be used as a basis for measuring drag.  More examples (Wing area vs total wetted surface area including fuselage):

Fw-190A8:  197/735 = 26.8%

P-51D:  235/882 = 26.6%

Looking at the length of fuselages of F4u and George will show this trend applies there too!


So when we see a HP output of 1620 at 20k for the Homare 21 engine (a hard number), is that an estimated value also?  It must be, for even the Ki-84 isn't much faster than a Hellcat at 20k with the same engine as the George.  When you put the George's 370 mph speed with the Frank's 385 or so, it makes sense.  It looks to me that the engine actually only put out 1300 hp at 6000m (from a reference to an Homare 22, which is probably very similar to the 21 as sea level output is practically the same).

[This message has been edited by wells (edited 11-30-1999).]

Offline Vermillion

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The "Curious George" or a "Castrated George" ?
« Reply #12 on: December 01, 1999, 08:50:00 AM »
Thats all I ask Pyro   Thats all I ask.

FYI if I go back and change the numbers you mention, it doesn't really change the relative rankings (except to actually fix the admitted 109 vs P51 speed problem), just the absolute numbers. And I even stated up front the numbers were only useful for a relative comparison, not of quality to build a FM.

One small comment though   Just because an airplane in the sim get kills (your reference to K/D ratio) don't mean that it is correct or that it represents the aircraft accurately. It might just mean that it has big friggin guns (BFG)  

Thanks for taking the time to repond !

Oh.... and about that P-63, two weeks right?


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Vermillion
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[This message has been edited by Vermillion (edited 12-01-1999).]

214CaveJ

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The "Curious George" or a "Castrated George" ?
« Reply #13 on: December 01, 1999, 09:32:00 AM »
Pyro-
lotta good info there, quite educational, thanks =)

On the Corsair, I dinnae want a super-kill-em-all bird, just one that flies as realistically as possible.  And there just so happens to be guy who's flown one (though a license-built Goodyear version) and is restoring another flying AH =)

Ya'll keep up the good work

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Offline jedi

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The "Curious George" or a "Castrated George" ?
« Reply #14 on: December 01, 1999, 03:45:00 PM »
One thing that must be considered is that NO computer-game flight model is going to be absolutely perfect at replicating the performance of every aircraft.

Do you take all the numbers for one aircraft, work backwards to the equations, and then assume that those equations will automatically yield the proper numbers for another aircraft?  Do you use the dreaded "table-based" modeling of AW (in)fame?  If you do, you can kiss your beloved "force-based, six-degrees-of-freedom" flight model quirks, landing, takeoff, torque, stall, and spin behavior goodbye.  Or do you use the most comprehensive model you can create, model as many "features" as you can, put in the most "reliable" information as to drag, airfoils, weights, and so on, and hope that your "hi-fidelity" model yields the correct results?

At some point, Pyro has to choose which aircraft physical data to "feed" to the flight model.  Once that's done, the aircraft performs a certain way.  If it matches HIS data, I'd have to say that the MODEL is correct.  If it doesn't, then either the model is at fault (and will be for every airplane modeled) or the data used for weight, drag, power, etc must be flawed.

IMO it's still early days yet to be picking apart INDIVIDUAL aircraft quirks, when presumably the flight model itself is not in its final form.  As for which data is "right," well, if you can convince Pyro that what you've got is "better" than what he's using, then by all means do so, and we'll get a more accurate plane out of it.  Otherwise, at some point you may just have to live with a "95-percent solution" if you want to have actual physics modeling instead of performance tables.

Just MHO of course  

--jedi