Author Topic: Spit XVI - please reconsider  (Read 3579 times)

Offline Kev367th

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Spit XVI - please reconsider
« Reply #90 on: August 05, 2005, 09:53:03 AM »
Yes, the pilots did the same with the VIII. Called it VIIIb.
Was because of the screw up with wing designations.

Originally
'a' wing - 8x.303
'b' wing - 2x20mm + 4x.303
'c' wing - 4x20mm
'e' wing - 2x20mm + 2x50 cal

Now when the 'b' wing was modified to allow ord and mixes of guns people started calling it the universal 'c' wing, hence the mixup.
More correctly would have the 'improved b wing'.

This is why I said earlier strictly speaking there never was a IXc.
99% of the time a 'c' wing Spit will actually be an improved 'b' wing wing.
99%?
Well there were some Spits with 4x20mm that can be correctly called a 'c' wing Spit.
« Last Edit: August 05, 2005, 09:57:18 AM by Kev367th »
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Offline Kev367th

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Spit XVI - please reconsider
« Reply #91 on: August 05, 2005, 11:04:23 AM »
Was thinking about the whole 25lbs / climb thing.

Wouldn't this actually create better fights?
Think about it.
Usually a large hoard arrives at a field with the defenders still climbing up to them. So it turns into a beat the defenders lower till they are on the deck getting buzzed by loads of cons.

With the XVI, they'd have the possibilty of using all the WEP to get to decent alt to intercept them on a more equal basis.
Oops, just said equal, don't want equal do we ;)
Remember - once WEP has gone it is just a standard Merlin 66 - there will be no XVI cruising round the MA for hours on end at 25lbs boost.

OK so it may mean the XVI becomes the Spit of choice for initial base defence until others can get there.

Would still like to find more climb charts for thr XVI to either confirm or debunk the only one we have at the moment. That rate of climb puts it on par with a Spit F.21.
« Last Edit: August 05, 2005, 11:17:21 AM by Kev367th »
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Offline Guppy35

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Spit XVI - please reconsider
« Reply #92 on: August 05, 2005, 11:11:21 AM »
Quote
Originally posted by Kev367th
Yes, the pilots did the same with the VIII. Called it VIIIb.
Was because of the screw up with wing designations.

Originally
'a' wing - 8x.303
'b' wing - 2x20mm + 4x.303
'c' wing - 4x20mm
'e' wing - 2x20mm + 2x50 cal

Now when the 'b' wing was modified to allow ord and mixes of guns people started calling it the universal 'c' wing, hence the mixup.
More correctly would have the 'improved b wing'.

This is why I said earlier strictly speaking there never was a IXc.
99% of the time a 'c' wing Spit will actually be an improved 'b' wing wing.
99%?
Well there were some Spits with 4x20mm that can be correctly called a 'c' wing Spit.



Pilots referred to the Spitfire LFIX as the Spitfire IXB.  It had nothing to do with the wing armament in that case.  It was an unofficial designation.

The C wing on the Spitfire V was a complete redesign to allow for the  three different set ups of 8 303s, 2 20mm and 4 303s or 4 20mms.  That made it "Universal"

The A wing on a Spitfire V could only hold  8 303s.  The B wing on the Spitfire V could only hold 2 20mm and 4 303s.

When the VII, VIII and IX got moving they already had the Universal wing of the Spitfire Vc.  They were not going to go backwards and have the two previous wing designs produced anymore as the Universal wing could handle all three set ups.

This in turn lead to there being no designation for the Universal wing on any other Spits beyond the Spitfire V.

Only later when the E wing was developed that was only 2 20mm and 2 .5MGs did they add the E designation to the IX and XIV.

The XVI did not have the E designation added as the XVI was only produced with the E wing set up.

Confusing isn't it :)

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Offline Karnak

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Spit XVI - please reconsider
« Reply #93 on: August 05, 2005, 11:13:14 AM »
Kev,

That would be better in that very narrow and specific circumstance.

However, imagine the cons are arriving in Mk XVIs with WEP unburned.  Not even any more is it.

The concern, if the climb is 5700ft/min, is that we'd have a fighter with better acceleration than anything other than an Me163, roll rate of a Ki-84, speed of an F4U-1, the turn capability of a Spitfire only slightly less and good firepower.  That is a very potent package.  From your posts it seems to me that you focus on top speed too much.  In a dogfight acceleration is, in my experience, much more important.  Who cares if that P-51D's top speed is 13mph faster than your Spit XVI's when it takes him a 45 seconds to go from 200mph to 300mph and it takes you 25 seconds to do the same.  He'll never live to reach 367mph.  You'll either force him to manuever, thus preventing him from getting there, or kill him.

Now, if the real climb is less, and I'd not be surprised if it were, then the issue may not be present at all.
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Offline Kev367th

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Spit XVI - please reconsider
« Reply #94 on: August 05, 2005, 11:36:32 AM »
Understood Karnak -
But it's almost like saying we shouldn't have
  • aircraft because it may stand a good chance of killing the late war speed demons.


As someone showed even with WEP its still only the 12th fastest aircraft compared to the rest.
I know I concentrate on speed, but you should know in the MA speed is everything.
Knock it down to 18lbs boost and it falls further behind (-24mph) the speed demons.
I think all most of us wanted was a Spit that 'may' stand a chance of catching these guys without going to more Griffon engined (certainly perked) aircraft.

Just seems we are destined never to get a free Spit at full performance because they are too good.
Lol, the Brits produced an aircraft thats too good to compete with the late war speed demons, compliment I guess.

Yeah I think it's lower, might be worth comparing a different clipped Spit to non-clipped Spit and extrapolating what it may be.

[edit] Went thru the clipped wing spit thread, no graphs on climb vs standard wing :( .

Did find something on web that said intial rate of climb for a XVI was 4100fpm, but no mention on 18/25 clipped/unclipped.

AH HA - Clipping results in loss of climb of approx 160-200fpm at all alts, would assume the 160 is at low alts, 200 higher alts.
« Last Edit: August 05, 2005, 12:05:39 PM by Kev367th »
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Offline Kev367th

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Spit XVI - please reconsider
« Reply #95 on: August 05, 2005, 12:11:29 PM »
RE: Clipping.

As previous post loss in climb 0f 160-200 fpm

Doesnt mention specific alts (tested up to 20k) but assuming it's reasonably linear -

0ft - -160
5000ft - -170
10000ft - -180
15000ft - -190
20000ft - -200

Would have to extrapolate for alts >20000 (-10fpm per 5000ft?)

You should definately read that report again, seems full of typos -
Mentions 160 grade fuel?
An average increase of 1100fpm, yet the MAX gain is only 800fpm.

Didn't the XVI carry slightly more fuel than the IX, and wasn't it heavier?

I think we need another source!
Even sent an email to Rolls Royce history dept:)
« Last Edit: August 05, 2005, 01:08:32 PM by Kev367th »
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Offline Karnak

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Spit XVI - please reconsider
« Reply #96 on: August 05, 2005, 01:47:02 PM »
Quote
Originally posted by Kev367th
Understood Karnak -
But it's almost like saying we shouldn't have
  • aircraft because it may stand a good chance of killing the late war speed demons.


As someone showed even with WEP its still only the 12th fastest aircraft compared to the rest.
I know I concentrate on speed, but you should know in the MA speed is everything.
Knock it down to 18lbs boost and it falls further behind (-24mph) the speed demons.
I think all most of us wanted was a Spit that 'may' stand a chance of catching these guys without going to more Griffon engined (certainly perked) aircraft.

The thing is that in my experience speed isn't everything.  You want adequate speed, but once that is obtained acceleration, manueverabilty and E retention are a bigger factor.  If the climb is 5700ft/min only the La-7 might have a realistic shot of escape after a tangle that the La-7 pilot determines he can't win.  The Spit will simply out sprint all others, and probably the La-7 as well.

I don't think it would have a chance against the speed demons, I think it would dominate them.  And then, when 20% of the kills each tour are Spit XVI it would be perked.

And think what it would do to something like a P-38, C.205, Bf110G-2, Mosquito Mk VI, Ki-61-I-Tei, Bf109G-6, P-47D, ect, ect.  Those would all be absolutely helpless before it.  You have to think about it's total impact, not just the impact on a few select aircraft.  That is Pyro's concern.
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Offline Angus

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Spit XVI - please reconsider
« Reply #97 on: August 05, 2005, 01:55:45 PM »
Hehe, the XVI is THE knifefighter, but would be endangered by much faster planes, or other Spits.
Would be a headache for the llw down guys, and that time to alt is really impressive.
Well, that's the Spitty. RL Spit is too good for AH :D
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Offline Squire

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« Reply #98 on: August 05, 2005, 02:08:47 PM »
In regards to the XVIs climb rate, im not so sure whats shocking, its a Mk IX with the hp of a heavier XIV ( @ 2000) when its boosting +25. Its going to be a freaking rocketship...

Even a LF IX on 100 octane is impressive at +18 lbs.

Albeit thats only on WEP for a limited time.
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Offline Kev367th

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« Reply #99 on: August 05, 2005, 02:14:08 PM »
Thats it Squire limited to 5 mins, does everyone expect XVI flying the MA at 25k+ (lol, you know it will happen) for hours on end at 25lbs?
5 freakin minutes.

Anyway as I said in other thread trying to find more data to either confirm or debunk the ONLY source we have at the moment.
I have an unconfirmed source that puts initial climb at 4100 NOT 5700fpm.

Apart from that if the figures are to belived that 5700fpm is only up to 5000ft.
Very little diff at 10k between 18/25 boost
15k and up theres no diff between 18/25 boost.

for 18 boost if the source is accurate

0 - 4960fpm
5000 - 4970fpm
10000 - 4280fpm
15000 - 4280fpm
20000 - 3730fpm
25000 - 2950fpm
30000 - 2200fpm

Karnak - I wish we had acceleration figures just to see if what is being assumed is true.
« Last Edit: August 05, 2005, 03:23:57 PM by Kev367th »
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Offline Kurfürst

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Spit XVI - please reconsider
« Reply #100 on: August 06, 2005, 09:33:38 AM »
Quote
Originally posted by Guppy35

They started using the 150 octane and 25+ boost in May 44 so there was an entire year where  IXs and XVIs were operating at the higher boost before the war ended.  Clearly 2 TAF birds got the fuel too so the ground attack Spits were using it.

Dan/CorkyJr


According the Neil Stirling, only 2, then 3 MkIXs Squadrons were operating at +25lbs boost in 1944.

The other 34 MkIX Sqns operated at the normal +18lbs boost with 100 octane fuel.

The 2nd TAF did not get 150 grade fuel until 1945, and until then, operated at max. 18 lbs.
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Offline Kurfürst

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« Reply #101 on: August 06, 2005, 09:40:09 AM »
Posting it here, too, about the +25 lbs ROC...


The 5700 fpm data at +25lbs is believable, if you know how it was arrived.

The 5700 fpm was measured in Spit IX test and noted for the VIII when the coolant radiator flaps were overridden and force-closed. With the standard way of measuring climb rate in other spitfire tests, with the radiators open, they measured 5080 fpm, a believable figure compared to the 4650 fpm measured under similiar conditions but at +18 lbs boost at SL.

Force-closing the rads during the test of course reduced drag and increased performance, but was highly theoretical, given that the radiator flaps were automatically operated and the pilot could not set them manuall on the MkIX/XVI - they would open very soon after the temperature started to rise to compensate (they were thermostatically controlled). Hence why the RAF always measured ROC with open radiators, with the exception of these tests.

See here : http://www.spitfireperformance.com/jl165.html


Bottom line, the +25 lbs Spit9/16 was good for around 5100 fps under normal, comparable conditions to other planes. Of course, other could as well increase climb rate by manipulating radiators, and reducing drag, with similiar limiations.
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Offline Karnak

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« Reply #102 on: August 06, 2005, 12:11:42 PM »
Quote
Originally posted by Kurfürst
Posting it here, too, about the +25 lbs ROC...


The 5700 fpm data at +25lbs is believable, if you know how it was arrived.

The 5700 fpm was measured in Spit IX test and noted for the VIII when the coolant radiator flaps were overridden and force-closed. With the standard way of measuring climb rate in other spitfire tests, with the radiators open, they measured 5080 fpm, a believable figure compared to the 4650 fpm measured under similiar conditions but at +18 lbs boost at SL.

Force-closing the rads during the test of course reduced drag and increased performance, but was highly theoretical, given that the radiator flaps were automatically operated and the pilot could not set them manuall on the MkIX/XVI - they would open very soon after the temperature started to rise to compensate (they were thermostatically controlled). Hence why the RAF always measured ROC with open radiators, with the exception of these tests.

See here : http://www.spitfireperformance.com/jl165.html


Bottom line, the +25 lbs Spit9/16 was good for around 5100 fps under normal, comparable conditions to other planes. Of course, other could as well increase climb rate by manipulating radiators, and reducing drag, with similiar limiations.

Insteresting.  Now that you mention it, I vaguely remember reading something about forced closed radiators during some tests else where.

I have been trying to think of how adding 400hp added 1200ft/min of climb.
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Offline Nashwan

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Spit XVI - please reconsider
« Reply #103 on: August 06, 2005, 12:39:54 PM »
Quote
The 5700 fpm was measured in Spit IX test and noted for the VIII when the coolant radiator flaps were overridden and force-closed. With the standard way of measuring climb rate in other spitfire tests, with the radiators open,


What Isegrim isn't saying, of course, is that the other tests he's talking about had radiators forced open.

Other aircraft, like the 109, had radiators set at certain positions for certain tests. For example, most German speed tests were done with radiators almost closed, something that could only be done for short periods. In AH, though, which doesn't model complex engines/cooling settings, the 109 can maintain such speeds for 10 minutes, in other words the AH 109 can maintain closed radiators/maximum boost for 10 minutes, something the real life 109 couldn't do.

The Spitfire had automatic radiators, that would open when the coolant temperature reached 115 c. Below that temperature they would close (closed on the Spitfire actually means half open, as the radiators cannot fully close)

So, what Isegrim is arguing for is climb figures for the Spitfire with radiators fully open. 109 figures are given with radiators half open, 109 speed figures with radiators almost fully closed.

AH doesn't model the extra drag from opening radiators, why should it do so for the Spitfire?

From cooling trials of the Spitfire LF IX, running at 25 lbs boost, after climbing at maximum power from 2,000 ft, overheating occured at 25,000 ft, under temperate summer conditions. That takes 6 minutes 17 secs, AH would of course have cut the power long before this, before the overheating would have occured. In fact, AH would have cut the power for a 25 lbs Spitfire LF IX at about 21,000 ft.

In normal service, the Spitfire would begin a climb with radiators closed, they would only open some time into the climb, this is modelled in AH by the system of automatically shutting off WEP after a pre determined time.

That's how it works for all aircraft in AH, having an extra penalty of forcing the radiators open on the Spitfire would be unfair unless the same rules are applied to other aircraft.

Quote
I have been trying to think of how adding 400hp added 1200ft/min of climb.


It's actually about 1,000 ft/min.
An extra 1,000 ft/min for the Spitfire LF IX would be about 20 - 25% better climb rate, 25 lbs boost added 25% more power. Weight was the same.

Online MiloMorai

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Spit XVI - please reconsider
« Reply #104 on: August 06, 2005, 12:52:05 PM »
JL165 had been around for some time before the test took place. From 27-3-43, with the testing starting in Oct 43.

Karnac, you should look at this link, http://www.spitfireperformance.com/bs543.html which gives data for rad flaps open (as noted on the chart). 4640 to 4700 ft/m (SL to 7000ft) See this link to show what the RoC was over 18lb, http://www.spitfireperformance.com/jl 165rr.html Averging 800ft/min to 10,000ft. (the 110 number and the 190 number are wrong if you look at the rate in the other link)

This gives a 5400 to 5500ft/m RoC, rad flap open.