Author Topic: F6F Vs. F4U  (Read 11862 times)

Offline Widewing

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F6F Vs. F4U
« Reply #45 on: September 02, 2006, 10:01:14 PM »
Quote
Originally posted by F4UDOA
I am using NACA document 829.

The Clmax was reduced in the F4U from 2.30 to 1.88 with full flaps (50 degrees deflection). You can see the F6F Clmax is marginally higher with Full flaps. Airplane #1 next to them does not have any flap deployed.

Dean's numbers have the F6F Clmax around 2+ without flaps.


Report 829 states that the sharp-edged spoiler installed to reduce wing drop is what lowered the F4U's CLmax, not the use of flaps.

"The maximum lift coefficient of the airplane, however, was reduced from 2.30 to 1.88 by the sharp leading edge."

Also, if you compare figures 14 and 15 with the figure you posted, you can see the CLmax change associated with full flap deployment on both the F6F-3 and F4U-1. CLmax numbers in figure 14 and 15 represent 0 degrees of flaps.

My regards,

Widewing
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline Widewing

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F6F Vs. F4U
« Reply #46 on: September 02, 2006, 10:05:53 PM »
Quote
Originally posted by bkbandit
wait, cannons on f6f?? did it have them?? i noe the raf for some reason reguned our american planes, there p51 had cannons(why dont we) did there f6f have cannons??  Not that i want them, personally i think the 6 50s are a better air to air weapon.


All F6F-5s were engineered to install a pair of 20mm cannon. However, they were only installed on F6F-5N night fighters, and many were removed and replaced by Browning .50 cal MGs as the muzzle flash of the cannons would cause a loss of night vision. You can find many photos of F6F-5Ns armed with only machine guns... Pilots liked the added firepower, but you can't shoot what you can't see. So, many had MGs retrofitted.

My regards,

Widewing
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline F4UDOA

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F6F Vs. F4U
« Reply #47 on: September 02, 2006, 11:12:29 PM »
Quote
Report 829 states that the sharp-edged spoiler installed to reduce wing drop is what lowered the F4U's CLmax, not the use of flaps.


Widwing,

I wasn't saying that it was because of the use of the flaps. I was responding to Shuckins implying that the Clmax of the F6F without flaps is over 2.0 which did not exist to my knowledge of any WW2 fighter. But Dean's list of Clmax numbers is just way off the mark. Because of that his turn index is way off.

If you put the right data into that calculation the results are very different.

Also it should be noted that much of the reason that the F6F wing had a higher Cl than the F4U was the intial roughness of the F4U wing which was later corrected. So the Cl max increased from the NACA report going forward.

Offline Saxman

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« Reply #48 on: September 02, 2006, 11:40:10 PM »
I thought I remember reading somewhere the unreliability of the American-produced version of the Hispano caused the military to largely pull the 20mm except for a handful of aircraft.
Ron White says you can't fix stupid. I beg to differ. Stupid will usually sort itself out, it's just a matter of making sure you're not close enough to become collateral damage.

Offline Widewing

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« Reply #49 on: September 02, 2006, 11:56:10 PM »
Quote
Originally posted by F4UDOA
Widwing,

I wasn't saying that it was because of the use of the flaps. I was responding to Shuckins implying that the Clmax of the F6F without flaps is over 2.0 which did not exist to my knowledge of any WW2 fighter. But Dean's list of Clmax numbers is just way off the mark. Because of that his turn index is way off.

If you put the right data into that calculation the results are very different.

Also it should be noted that much of the reason that the F6F wing had a higher Cl than the F4U was the intial roughness of the F4U wing which was later corrected. So the Cl max increased from the NACA report going forward.


Well, it seems that NACA was trying to isolate the wing performance without the influence of the prop. When the prop was "idling", the CLmax increased. I suspect that at max RPM, low pitch, CLmax will increase substantially more.

I also believe that NACA claims that the spoiler strip presented a trade-off. A significant reduction of CLmax in exchange for much better handling near stall speed. Most would agree that it was a good trade.

This report shows that the F6F has a higher CLmax with and without flaps, but does not demonstrate the huge difference shown by Dean. Indeed, the differences were not dramatic, just as they are not far apart in the game... Which is to HTC's credit.

Also in the report is a description of the F4U and F6F wing. It seems that the F4U wing was very rough, with many panels and gaps. When taped up, the CLmax improved. Likewise for the F6F, but to a somewhat lesser degree. However, since both represented fleet aircraft, neither will be treated to taping and added fillets in service. When we look at the P-51 tested, we see that the wing is much cleaner. This is what one would expect as the P-51 wing doesn't fold. Of course, the P-51 has a considerably higher wing loading than the two Navy fighters, which is more significant IMHO.

My regards,

Widewing
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline Widewing

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F6F Vs. F4U
« Reply #50 on: September 03, 2006, 12:04:38 AM »
Quote
Originally posted by Saxman
I thought I remember reading somewhere the unreliability of the American-produced version of the Hispano caused the military to largely pull the 20mm except for a handful of aircraft.


F6Fs certainly had issues with the cannons jamming. However, most of the time careful deburring, stoning of bolts and reassembly cured these ills. Tillman writes about these issues in his Hellcat book.

Most were removed because they were delivered without flash suppressors. Some squadrons had the carrier's machine shop manufacture suppressors from bar stock, but the majority simply removed the cannons and installed .50 cals until they received factory suppressors.

My regards,

Widewing
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline HoHun

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F6F Vs. F4U
« Reply #51 on: September 03, 2006, 04:53:50 AM »
Hi Widewing,

>Well, it seems that NACA was trying to isolate the wing performance without the influence of the prop.

Fortunately, that yields about the same Clmax we get in a high speed turn when the effect of the propeller slipstream is relatively small.

I'd take the numbers from the figures 14/15 you pointed out as good data on the relative turning capabilities.

Plugging them into my spreadsheet, I get the following sustained turn rates at 1000 m:

16,12 °/s for the Fw 190A-5 @ 3989 kg, 1.32 ata, 2400 rpm (Clmax 1.21)
16,62 °/s for the F6F-3 @ 12,740 lbs, 60" Hg, 2700 rpm (Clmax 1.29)
16,38 °/s for the F4U @ 12,470 lbs (Clmax 1.17)
17,15 °/s for the Fw 190A-5 @ 3989 kg, 1.42 ata, 2700 rpm (Clmax 1.21)

Hm, suprisingly, the aircraft are rather close and the Fw 190 on emergency power actually comes out best. The Navy fighters were flown at a slightly reduced weight compared to the figures I used, but I'm not sure that accounts for the difference. I'll have to analyse that later.

>This is what one would expect as the P-51 wing doesn't fold.

It might also be the result of trying to build a laminar-flow wing, which required greater attention to surface quality.

Regards,

Henning (HoHun)

Offline F4UDOA

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F6F Vs. F4U
« Reply #52 on: September 03, 2006, 08:39:04 AM »
HoHun,

You F4U weight is a few hundred pounds high. Try 12,175 for a fully loaded -1D. Most listings are closer to 12,000lbs even.

Also those Clmax numbers are with prop removed and no slipstream. The F4U Clmax calculated with no power and no flaps moves up to 1.49. The F6F I am not sure because of CAS error.

Check this.







Offline HoHun

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« Reply #53 on: September 03, 2006, 01:33:55 PM »
Hi F4UDOA,

>You F4U weight is a few hundred pounds high. Try 12,175 for a fully loaded -1D.

Ah, I accidentally used the F4U-1C weight instead of the -1D weight from the same chart!

>Also those Clmax numbers are with prop removed and no slipstream.

For turning purposes, that's the one that gives the most realistic results.

(I also found some other Focke-Wulf data. There is a large variance in Focke-Wulf data, I used a dataset yielding 666 km/h @ 6.2 km which results in a slightly worse turn rate than I quoted previously.)

Corrected comparison at 1 km:

16,11 °/s for the Fw 190A-5 @ 3989 kg, 1.42 ata, 2700 rpm (Clmax 1.21)
16,62 °/s for the F6F-3 @ 12,740 lbs, 60" Hg, 2700 rpm (Clmax 1.29)
16,83 °/s for the F4U-1D @ 12,175 lbs (Clmax 1.17)

At 8 km:

7.15 °/s for the F6F-3 @ 12,740 lbs, 60" Hg, 2700 rpm (Clmax 1.29)
7.75 °/s for the Fw 190A-5 @ 3989 kg, 1.42 ata, 2700 rpm (Clmax 1.21)
7.75 °/s for the F4U-1D @ 12,175 lbs (Clmax 1.17)

(The Hellcat might be a bit inaccurate, I didn't fully understand all the historical data and its apparent contradictions. I'm also using the weight data from the F6F-5 for the F6F-3 with water injection though the latter might be lighter - or not.)

Regards,

Henning (HoHun)

Offline gripen

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F6F Vs. F4U
« Reply #54 on: September 03, 2006, 04:29:34 PM »
Quote
Originally posted by HoHun

[F4UDOA]>Also those Clmax numbers are with prop removed and no slipstream.

For turning purposes, that's the one that gives the most realistic results.


Actually not, the flight envelope chart as F4UDOA posted above gives far more more realistic results (assuming that weight and IAS/TAS conversions are accurate).

gripen

Offline bkbandit

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F6F Vs. F4U
« Reply #55 on: September 05, 2006, 08:46:02 AM »
heres somethin that hit me yesterday, i was flying fm2 and it is way more roughed then f6f, arent the supposed to be the same in the duribility department. I was at 186(took 2 hours for the bishops to take the base away from the nites, a very depressing site) and fm2 is slow but the turn rate and duribilty let me kill tons of hurris ju88s 110 etc. Im not to sure about f4u but i noe f6f was know for absorbing retarded amounts of damage then roll over and bag a kill.

Offline Saxman

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« Reply #56 on: September 05, 2006, 10:51:27 AM »
bkbandit: Even P-47 pilots admitted that the F4U was by far the toughest single-engine fighter the Americans produced. However I routinely have stabs, wing parts, and the entire tail blown off by long-range pings from machine gun fire (d600-1000).

For that matter, I've absolutely UNLOADED (I'm talking at LEAST 100-200 rounds) within convergence into the engines of Spits, HO-icanes and Mustangs and watched them fly off without any sign of damage, and yet one or two pings will kill the engine on a Hog? The R-2800 was supposedly one of the most rugged and reliable aircraft powerplants of the war and was known to continue to operate despite having whole cylinder heads completely blown off, but here one hit is all it takes to cause a fatal oil leak while the far less durable Merlin keeps humming.
Ron White says you can't fix stupid. I beg to differ. Stupid will usually sort itself out, it's just a matter of making sure you're not close enough to become collateral damage.

Offline bkbandit

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« Reply #57 on: September 05, 2006, 11:43:28 AM »
they realllllyyyyy need to the fix this, they need to up the armor or something, the american planes werent werent a agilie but made up for it 2 fold with the armor.

Offline HoHun

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« Reply #58 on: September 05, 2006, 04:21:22 PM »
Hi Saxman,

>bkbandit: Even P-47 pilots admitted that the F4U was by far the toughest single-engine fighter the Americans produced.

Do you perhaps have the quote ready? That would be quite interesting :-)

However, with regard to reputation, I'm afraid it's not a very accurate representation of reality.

If you look at the US Navy statistics that were prepared just after WW2 based on their total combat experience, the one aircraft type that could really take more flak than any other and still come home was the Douglas SBD.

I don't know whether people who read other books than I did share this impression, but I'd never have thought it was such a tough aircraft based on all those books I had read on WW2 air combat. Sure, one always reads that the pilots were unhappy about the SB2C and liked the SBD much better, but that might have just indicated that the SB2C really had a lot of problems ...

So, it's always better to try and find some data to cross-check the reputation now and then ;-)

Regards,

Henning  (HoHun)

Offline Widewing

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F6F Vs. F4U
« Reply #59 on: September 05, 2006, 05:30:47 PM »
Quote
Originally posted by HoHun
Hi Saxman,

>bkbandit: Even P-47 pilots admitted that the F4U was by far the toughest single-engine fighter the Americans produced.

Do you perhaps have the quote ready? That would be quite interesting :-)

However, with regard to reputation, I'm afraid it's not a very accurate representation of reality.

If you look at the US Navy statistics that were prepared just after WW2 based on their total combat experience, the one aircraft type that could really take more flak than any other and still come home was the Douglas SBD.

I don't know whether people who read other books than I did share this impression, but I'd never have thought it was such a tough aircraft based on all those books I had read on WW2 air combat. Sure, one always reads that the pilots were unhappy about the SB2C and liked the SBD much better, but that might have just indicated that the SB2C really had a lot of problems ...

So, it's always better to try and find some data to cross-check the reputation now and then ;-)

Regards,

Henning  (HoHun)


Henning, here's the specific quote you are referring to, from page 78 and 79:

a) Loss rates to enemy A/A were highest in 1942 and generallv lowest in 1943. increasing slightly from then until the end of the war. The 1942 rates reflect the predominance of large enemy warships among the targets for that year, figures for 1943 and subsequent years the relatively lower but increasing effectiveness of Japanese land A/A. Actually enemy A/A material improved and increased in volume at a far greater rate, but this trend was offset by the improved performance characteristics of Naval aircraft, and improved tictics against A/A.

(b) Loss rates for carrier-based aircraft were consistently higher than for land-based aircraft, despite inclusion in the latter of the relatively vulnerable VPB. The reason is that land-based aircraft generally were assigned to attack the less well-defended rear area targets, already well beaten down by the carrier forces, such as those in the Marshalls and Philippines. Also their campaigns against such heavily defended targets as the Rabaul area were of long duration, and by the later stages enemy A/A guns had been greatly reduced in number and ammunition supplies
depleted. Carrier aircraft, on the other hand, were constantly reaching out toward the most heavily defended targets, pressing their attacks close to wipe out such small and vital targets as grounded aircraft, warships and merchant vessels, and seldom staying long enough to enjoy the benefits of the reduced A/A defenses resulting from their attacks.

(c) The lesser effectiveness of enemy A/A against our land-based planes did not result from an appreciably lower rate of hits per sortie attacking defended targets, but from generally lower lethal effect of hits. A smaller percentage of the land-based planes hit by A/A was lost. In part, also the lower rate of losses for land-based planes reflected the extensive use of the less vulnerable SBD, while the carriers were shifting to the highly vulnerable SB2C.

(d) The SBD, carrier-based or land-based, had consistently the best record of any plane model. It generally received slightly less hits per sortie than other planes, and in addition had the lowest ratio of losses to hits of any single-engine plane.

(e) The F6F appears to have had considerable advantage over the F4U when flown under the same conditions. Receiving about the same number of hits per sortie in comparable operations, the F6F had a far lower rate of loss per plane hit.

(f) The TBM loss rate appears to have been lower than that of the SB2C. It received more hits per sortie, but showed greater ability to survive hits. Both SB2C and TBM were somewhat more subject to A/A loss than fighters.

Loss rates per 100 action sorties, by carrier type:

F6F:     .87  CV/CVL       .83 CVE
F4U:   1.46  CV/CVL      .90 CVE
FM:        0  CV/CVL         .48 CVE
SBD:    .68  CV/CVL         0 CVE
SB2C: 1.43  CV/CVL        0 CVE
TBM:   1.10  CV/CVL      .72 CVE

One should also note that the Navy states that the F6F was a more survivable fighter than the F4U. However, the small, rugged SBD was best at getting its crew home.

This next part is very interesting as well. From page 77:


In the case of F6F and F4U losses the bulk of those reported as destroyed by unidentified types, amounting to one-fourth of the total, have been prorated as noted in the footnote to the table. This, plus the errors in identification which may normally be expected in the action reports,
results in a decrease of accuracy which leaves something to be desired, but permits comparisons which are believed sufficiently near the truth to be of considerable value and interest, and are in any event the best available.

The result of comparing each pair of figures is to produce a combat ratio for air combat between each two models or types of planes involved - subject to the limitation on accuracy noted above.

The F6F appears to have shot down 15.5 single-engine Jap fighters for each F6F destroyed in combat with them. Against the Zeke the F6F ratio was over 13-to-1; against Oscar over 15-to-1; against Tojo (probably including a large proportion of misidentifications) over 31-to-1. Against
the most advanced types the F6F did less well: 8.5 to-1 against the Frank, Jack and George combined.

Unusual is the loss of 6 F6Fs in combat with Betty; however, with respect to enemy twin-engine planes as a whole the ratio was 66-to-1, and against all other bomber types combined is 225-to-1.

The F4U nearly matched the F6F performance during this period, with a 15-to-1 ratio against single-engine fighters, and 12-to-1 against Zeke. The F4U, however, included a relatively large number of obsolete Nates among its kills, and while its record against Oscar and Tony was superior to the F6F's, the F4U scored only 13-to-1 against Tojo, and only 6-to-1 against Frank, Jack and George combined.

The phenomenal FM leads all fighters during this period, with a 26-to-1 ratio over Jap single-engine fighters, only 2 losses sustained in destroying 87 Zekes, and only two losses in downing 194 bombers and miscellaneous types.

My regards,

Widewing
« Last Edit: September 05, 2006, 06:11:31 PM by Widewing »
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.