ub" Zemke liked the P-51 because it had great range, but he put one in a dive and when he pulled out he ripped the wings off that airplane--that was how he became a POW.
Originally posted by FUNKED1
Are those Johnson's words or Johnson's words as told to/filtered by/revised by Martin Caidin?
Originally posted by HoHun
Hi Widewing,
>Also, none of the German fighters were as rugged as a P-47.
I'd say Johnson lacked the basis for a fair comparison as he (hopefully) didn't shoot down enough P-47s to get a good average ;-)
>When I was badly shot up on June 26, 1943, I had twenty-one 20mm cannon shells in that airplane, and more than 200 7.92mm machine-gun bullets.
While this was impressive, I'd attribute that more to luck than to anything else. German experience was that the four-engined bombers went down after an average of 25 x 20 mm hits, and they were recognized as a lot tougher than the P-47. I'm sure some four-engined bombers returned safely with a multiple of these average 25 cannon hits, too.
>Johnson repeatedly claimed he could pull 72" of MAP and reported airspeeds of 470 mph TAS.
As the P-47 achieved it's top speed at very high altitude, the compressiblity error of the airspeed indicator was considerable. As this phenomenon doesn't seem to have been included in the typical WW2 fighter pilot training, I consider it likely that the 470 mph figure lacked the compressiblity correction.
Regards,
Henning (HoHun)
Originally posted by gripen
Water injection system in the P-47 worked automaticly (IIRC it started to work at given MAP say 54" or something).
Philipps shot down has been under discussion on various forums and AFAIK there is no consensus if it was Johnson or Bombers or someone else. At least AFHRA lists no claims for Johnson at March 2, 1944 (Mayer shot down).
gripen
Originally posted by HoHun
Hi Widewing,
At this altitude, running at 64" Hg boost yielding 2600 HP, the P-47D referenced in this report achieves a speed of 438 mph. Increasing boost to 72" Hg and power to 2900 HP would give us a calculated top speed of 454 mph.
Still very impressive, but far from the 470 mph you mentioned.
(Just how far? Well, the P-47D in question would need no less than 3200 HP to get there. And my calculations actually neglect the transsonic drag rise that at these speeds begins to make itself felt.)
In contrast, there seems to be little doubt about Hans Phillipp. Johnson shot down a Bf 110, and then, alone, attacked four Fw 190s. He obliterated the lead 190. Most historians concur that the facts reported by the Luftwaffe pilots flying with Phillipp and Johnson's account are in agreement in detail as well as location and time of day. I believe that historians Raymond Tolliver and Trevor Constable discovered this and verified it as fact.
My regards,
Widewing
apparently Luftwaffe loss records, indicate that Herr Philipp was shot up quite heavily by the American bombers he was attacking. If any P-47 finished him off, it was while his plane was already descending and out of commission. So the German version
On October 8, 1943, the 8th AF dispatched 156 bombers to targets in Bremen and Vegesack. The force was escorted by 250+ Thunderbolts from six different fighter groups.
The Stab Flight of the Geschwader heard Philipp announce a victory over a Thunderbolt. The last tranmission from him was: "Reinhardt, attack!" Feldwebel Reinhardt was Philipp's wingman on this day. He last saw the Kommodore's aircraft disappear in a cloud. Reinhardt was wounded after colliding with an enemy aircraft, but made a successful forced landing. Later that evening, the Geschwader learned that their Kommodore had been shot down and killed.
Originally posted by gripen
Here is couple NACA reports for additional info on R-2800. RM E6J08 (http://naca.larc.nasa.gov/reports/1946/naca-rm-e6j08/) is about pre-ignition limits with various fuels (28R is grade 100/130 and 33R is 110/145) and different spark-plugs (no water injection). Report 873 (http://naca.larc.nasa.gov/reports/1947/naca-report-873/) is about cooling of the R-2800 on high altitudes, it explains quite well why the P-47 tend to overheat at high altitude climbs. Overall it seems that 72" MAP might have been possible with right fuel (no water) but just for very short periods because overheating would have been pretty much instant without water injection.
Another interesting piece of data is ETO kill claim part (http://www.maxwell.af.mil/au/afhra/wwwroot/aafsd/aafsd_pdf/t167.pdf) of the USAAF statistical digest. Before January 1944 US fighters did not claim so many kills but after that claims steadily rise. Turning point appears to be the Big Week and after that claims still increased and continued in the same level until September. Basicly early P-47 operations did not affect a lot to Luftwaffe, seems that it was combined pressure on all fronts during summer 1944 which broke back of the Luftwaffe.
gripen
Originally posted by HoHun
Hi Widewing,
Before we lose sight of it:
>Then, how do you account for the P-47M-1-RE and P-47N-1-RE recording CORRECTED speeds of 475 and 467 mph respectively on 2,800 hp?
Where's you rspeed data from, and where's the evidence compressiblity correction has been applied to it?
Regards
Henning (HoHun)
Originally posted by HoHun
Hi Widewing,
>Once engaged, most pilots pushed everything forward and never even glanced at temp gauges until the fight was over.
Even with pushing everything forward, 72" Hg gives you no more than 300 extra HP (you only claimed 200 HP) over 64" Hg.
Starting from 2600 HP, that's around 10% of power gain, which yields around 3% of extra speed.
To get to 470 mph TAS, Johson's P-47 would have had to go at 456 mph TAS at standard power settings. And that below its optimum altitude, so the total top speed must have been even higher.
Where's your evidence for a 460+ mph top speed standard P-47D?
Regards,
Henning (HoHun)
Originally posted by HoHun
Hi Widewing,
>Please, stop being obtuse.....
Please stop being impolite. If you mistake thoroughness for obtuseness, that's your fault only. You were posting speed figures with no altitude given - quite obviously, that's useless for a detailed discussion.
I'm not being impolite whatsoever; but don't stand in the road because it's right around the bend.
This is your claim:
>>Then, how do you account for the P-47M-1-RE and P-47N-1-RE recording CORRECTED speeds of 475 and 467 mph respectively on 2,800 hp?
I'm quite ready to give you the benefit of doubt, but if you go and use capital letters, then I assume you have something to back up your claim.
First of all, it's not "my claim", these are established facts.
>If you need actual data, see Dean's "America's Hundred thousand", pages 282 and 283.
Do you mean this is your source? If it is, does it contain speed and power curves like the F4U-4 comparison?
That would be a useful basis for a thorough discussion of these aircraft. Your single figure quotes are not.
What did you think I meant? Yes, Dean provides speed, power and climb curves for many versions of the P-47D, as well as the P-47M and N. The F4U-4 is included. Dean's work is thorough (over 600 pages) and well respected. Invest in a copy.
My regards,
Widewing
Originally posted by HoHun
Hi Widewing,
>Someone's full of baloney, and I doubt that it was the USAAF's Experimental Engineering Division.
Try to concentrate on the question:
>>Where's your evidence for a 460+ mph top speed standard P-47D?
The laws of physics are pretty consistent, and the P-47D tested for the F4U-4 comparison is never going to get anywhere 475 mph for certain.
Either you prove the data for the tested P-47D is in error, or you prove my calculations are in error. Both could easily be possible, but I'm not going to believe it without positive proof.
And if you look at the P-47M and P-47N issue, you'll see that I've done nothing but asking questions. I've not made a single statement regarding their performance.
I'm mildy surprised that this was enough to make you lose your composition and resort to ad hominem statements. I'm not going to comment on your emotions - but please, keep them for yourself.
Regards,
Henning (HoHun)
Originally posted by leitwolf
Were modifications to engine and plane limited to the ETO or is reasonable to believe the Navy also had souped up F4Us and F6Fs ?
How'd they perform?
Originally posted by HoHun
Hi Widewing,
>Where did I state that a "standard" P-47D was a 460 mph fighter? Answer: Nowhere.
As I pointed out above, to get a standard P-47D up to 470 mph by a power increase from 2600 HP to 2900 HP, you need to start with a standard P-47D that makes 460 mph at optimum altitude.
Here is the data:
Critical altitude at 64" Hg: 27700 ft.
Critical altitude 72" Hg: 26500 ft.
Power at 26500 ft, 64" Hg: 2600 HP
Power at 26500 ft, 72" Hg: 2900 HP
Speed of a standard P-47D @ 2600 HP @ 26500 ft: 438 mph
Speed of a standard P-47D @ 2600 HP @ 27700 ft: 441 mph
Here's the result of my calculation:
Speed of a standard P-47D @ 2600 HP @ 26500 ft: 454 mph
Let's stick to Johnson's Jug.
P-47D-5-RE, R-2800-21
Power at 25,000 ft, 52" Hg: 2,000 hp
Power at 27,000 ft, 64" Hg: 2,300 hp
Those are the baseline numbers for Johnson's Thunderbolt as delivered per P&W data sheet for the -21 engine (ref. Bodie collection).
Gould was told by P&W that 72" Hg would generate 2,700 hp.
Baseline speed for the P-47D-5-RE was 433 mph @ 27,000 ft. on 2,300 hp.
Base your calculations on these numbers.
Either way, the fact that the P-47M attained 475 mph on 2,800 hp at 32,600 ft is a major stumbling block opposing your assertion that a P-47D-5-RE would require 2,900 to reach 470 mph when it has less drag and weighs 800 lbs less.
In the meantime, why don't you download the software, it's free. Then set up an account, the first two weeks are also free. This way, if we become annoyed with each other, there's some minimal recourse for revenge! LOLOLOLOL
No, that wouldn't be fair, I've been doing this a while. But, I would be willing to show you the "ropes" so to speak, to help shorten the learning curve (which is remarkably steep).
My regards,
Widewing