MiTasol
1st Lieutenant
and today Wiley got in the act as well. Non Sequitur by Wiley Miller for December 10, 2023 | GoComics.com
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Be sure to invent a plentifully available centrifugal supercharger that was fully available in 1941 but the Air Force was refusing to use it because they would rather lose than use a supercharger.I think I shall present a video about the merits of the P-39.
I have source material from an "expert" that I will use to present my point of view.
Anyone dares to refute my case will be blocked and I will belittle them in order to maintain my superior position.
Thus sayeth the Lord.
Y'all may be seated now.
Greg apparently had his feelings hurt by me regarding 'contrarian' views on his P-47 series regarding range, and now his recent 'breathless' breaking news about Fokker being the real engineering and production cadre that built P-51.
I am banned
View: https://www.youtube.com/watch?v=TWr50TP0CWc&t=4169s
For those that can wade into 58 minute region I am referred to as 'butt hurt' author trying to prop up sales.
The posts that lurched me into the evildooer image was a point by point fact citation for reasons the P-47 was Not held back from true place of glory on the first Schweinfurt mission.
But the posts that apparently put me into the evildooer/must be banned penalty box was a point by point rebuttal of his conclusions that NAA could ONLY have built the Mustang with heritage Fokker team acquired by General Motors team, then named General Aviation Manufacturing Corp.
His conclusion; Edgar Schmued was Fokker Design, someone I don't know (and not on NAA org chart) was the production genius and Van Breese was responsible for NAA test group - all Fokker in his words - and were the catalysts for North American ascension as a builder of airplanes. He did note that a couple of executives came from Douglas in a passing swipe.
Those (unmentioned) execs were Kindelberger (former VP of Engineering at Douglas - and daddy of DC-1 and DC-2), Atwood (Asst Chief of Engineering at Douglas and Chief of Structures), Smithson (Chief of Production) along with Ray Rice.
Atwood became Chief, Engineering at NAA, Rice joined later as Asst Chief of Engineering and Smithson became VP Production. This is mid 1934 Mangement team first at GAMC, then NAA on Jan 1 1935.
Sadly Greg has no clue regarding actual operations at Fokker when GAMC was formed, nor understanding what was important when the F.10 crash killed Knute Rockne in early 1931.
Apparently he believes that Fokker was leading Fokker Atlantic engineering that designed the F.10 to compete with Ford Tri-motor - not so. Robert Noorduyn who came to US with Fokker in 1921, left Fokker in 1929. Apparently Greg believes that Edgard Schmued developed his talent as an engineer under the tutelage of Fokker Engineers. Not so, Schmued was hired just as Fokker resigned after Rockne crash. The new Chief's of engineering replacements were first Thaden from Pittsburgh Aircaft, renamed Metalaire in 1931 and acquired by GAMC in 1931.
The Department of Commerce - Aeronautical Division as a result of Rockne crash investigation issued edict concerning comercial passenger aircraft. No more wooded structural members for flight safety (F-10 deemed to have failed due to rotted wood wing spar).
At this moment in time there were several F.10 and F-8 Universal still on the line that were sold offshore. The Fokker XO-27 was flying with several orders for YO-27 nad one request for bomber version XB-7 - which Schmued worked on as first assignment. ALL Fokker designs and production airframes were of wood spar with plywood covered wings, steel tube and linen fuselages.
The Thaden T-2 and T-4 were welded tube metal covered fuselage with steel truss spar/linen covered wing now being built by Pittsburgh Aircraft when acquired by GAMC. The Pilgrim 150 was a low cantilever, steel tube, alclad covered wing plus steel tube structure, Alclad fuselage.
The second new boss was Virginius Clark (Clark Y airfoil) and former Chief, Engineering that designed the Fairchild-American Pilgrim 150. The boss and the Pilgrim 150 came in December 1931 - to replace Thaden. The 150 was assigned GA-43. It first flew May 1932. There wil be more on this later if you can stay awake.
By end of 1931, all metal single and twin engine aircraft are flying or on the Drawing Board. Included are B-9, Boeing Model 200, Douglas DC-1 and Boeing 247. GAMC ses the handwriting on the wall - which is why Fokker is not only effectively DOA for future design in commercial aircraft due to lack of inhouse expertise in either sheet metal fabrication or aerodynamics, or airframe structure analytic for these new technologies.
Compare Fokker F.10 to the soon to be introduced Douglas DC-1. The DC-1 could take off an fly on one engine. ALL Alclad stressed skin construction, twin engines, 10 passenger, flaps, and retractable landing gear.
But a little bit about NAA. It was a Holding company specializing in commercial air transport companies and airframe manufacturers. It acquired Eastern Airlines, Curtis Aircraft, SperyGyroscope. 40% Douglas Aircraft, then Berliner Joyce Aircraft, then GAMC. When NAA acquired GAMC, it consolidated three plants to one at Dundalk MD with approximately 150-200 employees remaining - then in turn was acquired by GM and divested of all commercial airlines save Eastern Airlines.
Summary, end of 1934.
All Teteboro Fokker/GAMC/Pittsburgh Aircraft aircraft had been completed, delivered, shut down.
American Pilgram 150/GAMC GA-43 completed at Dundalk as first actual NAA aircraft produced.
Berliner Joyce new development complete, only new orders for SOC-1 & -2 steel, welded floats are in production.
Senior management team execs Kindelberger (CEO), Atwood (Chief Engineering), Smithson (VP Production), Bowen (Production Engineer and future X73 project manager, then Asst Plant Manager at new Dallas Plant), Hansen (Chief Project Enginering) - ALL from Douglas Aircraft
Key Managers and future key employees Rice (Asst Chief, Engineering) - Douglas Aircraft, Schlecher (Chief, Airframe structures) and Baldwin (Project Engineer) and Rudd (tool & die maker who rose to VP&Gen Mgr NAA Columbus Div) came from Berliner Joyce. Schmued (Preliminary Design engineer at acquisition by NAA (GAMC)
Summary-
Every design produced by NAA from XO-47 (GA-15) and BT-9 (NA-16) through XB-21, BC-1, Export Fighter NA-44, AT-6, NA-40, B-25, P-51 were led by Atwood through 1939, Rice thereafter. Douglas origins.
Schmued became Chief, Preliminary Design in 1939 wth first effort the P-509/X73. The project team was matrixed but still in Rice's Engineering department.
The Production quality was driven by Kindelberger with focus on speed, quality and ever decreasing Cost. Smithson and imbedded project engineers worked closely with Design with an eye towards actual process, and process flow.
Schmued's genius were two fold. A superb intuitive feel for aerodynamic shape and ability to pick/lead and manage a preliminary design team to a schedule the preliminary designs.
Schmued also the driver for the development and implementation of Projective Geometry of applied conical sections. He pushed, Roy Liming constructed the application to the Lofting developments.
Additional Oddities
Nothing from Fokker related to manufacturing excellence, specifically not 'butt joint quality production that Greg cites as reason speed advantage over Spitfire. Curiously he didn't mention wing or Meredith effect as 'other reasons' for performance but all those lay at feet of Smithson, and Rudd including flush rivet passion and development of 7075 skin deelopment and techniques later. Nothing from Fokker instituted filling, sealing, priming and painting wing to achieve surface quality independent of butt joint construction.
Nothing from Fokker instructed Ed horkey, Ashkenas, Beerer (all Cal Tech grads) in the fine art of airfoil development, aerodynamics, performance analyss or Meredith effect cooling system design - the latter a far larger difference maker than butt joint construction.
Nothing from Fokker introduced alclad sheet stress panel analysis and design that was cornerstone of NAA quality and strength.
Greg cites Van Breese as one of the Fokker trained giants that vaulted the Mustang into glory?
Well, interesting that Van Breesehad his own aircraft company 1927-1934. Breese Aircraft Company. last operating at Mines Field. He co-designed the Vultee V-1. Was bought out during the Vultee consilidation. He DID consult with Fokker Netherlands as a Demonstrator test pilot for Various Fokker designs attempting to gain a foothold in 1937. From that approximate time he was basically a full time test pilot and consultant including a stint with NAA in 1939/40 for the NA-44 and then 73X
Now for the other side of the ledger.
The rapidity and excellence of the first big success of NAA Design - the NA-16 BT-9 - had a large contingent of Dutch speaking shop team that worked 18x7 to get the prototpe done in time to win against Seversky. While the GA-43 was largely GAMC (Pilgrim) workers, the BT-9 was welded steel tube fuselage and fabric covering for fuselage and wing - right in the strike zone for the surviving Fokker (and Berliner Joyce) cadre that made the trip to Dundalk.
If anyone feels like stirring up some stuff in Greg's new video, you have my permssion to cut and paste. Warning - you may get banned.
Sincerely,
Butthurt
Greg apparently had his feelings hurt by me regarding 'contrarian' views on his P-47 series regarding range, and now his recent 'breathless' breaking news about Fokker being the real engineering and production cadre that built P-51.
I am banned
View: https://www.youtube.com/watch?v=TWr50TP0CWc&t=4169s
For those that can wade into 58 minute region I am referred to as 'butt hurt' author trying to prop up sales.
The posts that lurched me into the evildooer image was a point by point fact citation for reasons the P-47 was Not held back from true place of glory on the first Schweinfurt mission.
But the posts that apparently put me into the evildooer/must be banned penalty box was a point by point rebuttal of his conclusions that NAA could ONLY have built the Mustang with heritage Fokker team acquired by General Motors team, then named General Aviation Manufacturing Corp.
His conclusion; Edgar Schmued was Fokker Design, someone I don't know (and not on NAA org chart) was the production genius and Van Breese was responsible for NAA test group - all Fokker in his words - and were the catalysts for North American ascension as a builder of airplanes. He did note that a couple of executives came from Douglas in a passing swipe.
Those (unmentioned) execs were Kindelberger (former VP of Engineering at Douglas - and daddy of DC-1 and DC-2), Atwood (Asst Chief of Engineering at Douglas and Chief of Structures), Smithson (Chief of Production) along with Ray Rice.
Atwood became Chief, Engineering at NAA, Rice joined later as Asst Chief of Engineering and Smithson became VP Production. This is mid 1934 Mangement team first at GAMC, then NAA on Jan 1 1935.
Sadly Greg has no clue regarding actual operations at Fokker when GAMC was formed, nor understanding what was important when the F.10 crash killed Knute Rockne in early 1931.
Apparently he believes that Fokker was leading Fokker Atlantic engineering that designed the F.10 to compete with Ford Tri-motor - not so. Robert Noorduyn who came to US with Fokker in 1921, left Fokker in 1929. Apparently Greg believes that Edgard Schmued developed his talent as an engineer under the tutelage of Fokker Engineers. Not so, Schmued was hired just as Fokker resigned after Rockne crash. The new Chief's of engineering replacements were first Thaden from Pittsburgh Aircaft, renamed Metalaire in 1931 and acquired by GAMC in 1931.
The Department of Commerce - Aeronautical Division as a result of Rockne crash investigation issued edict concerning comercial passenger aircraft. No more wooded structural members for flight safety (F-10 deemed to have failed due to rotted wood wing spar).
At this moment in time there were several F.10 and F-8 Universal still on the line that were sold offshore. The Fokker XO-27 was flying with several orders for YO-27 nad one request for bomber version XB-7 - which Schmued worked on as first assignment. ALL Fokker designs and production airframes were of wood spar with plywood covered wings, steel tube and linen fuselages.
The Thaden T-2 and T-4 were welded tube metal covered fuselage with steel truss spar/linen covered wing now being built by Pittsburgh Aircraft when acquired by GAMC. The Pilgrim 150 was a low cantilever, steel tube, alclad covered wing plus steel tube structure, Alclad fuselage.
The second new boss was Virginius Clark (Clark Y airfoil) and former Chief, Engineering that designed the Fairchild-American Pilgrim 150. The boss and the Pilgrim 150 came in December 1931 - to replace Thaden. The 150 was assigned GA-43. It first flew May 1932. There wil be more on this later if you can stay awake.
By end of 1931, all metal single and twin engine aircraft are flying or on the Drawing Board. Included are B-9, Boeing Model 200, Douglas DC-1 and Boeing 247. GAMC ses the handwriting on the wall - which is why Fokker is not only effectively DOA for future design in commercial aircraft due to lack of inhouse expertise in either sheet metal fabrication or aerodynamics, or airframe structure analytic for these new technologies.
Compare Fokker F.10 to the soon to be introduced Douglas DC-1. The DC-1 could take off an fly on one engine. ALL Alclad stressed skin construction, twin engines, 10 passenger, flaps, and retractable landing gear.
But a little bit about NAA. It was a Holding company specializing in commercial air transport companies and airframe manufacturers. It acquired Eastern Airlines, Curtis Aircraft, SperyGyroscope. 40% Douglas Aircraft, then Berliner Joyce Aircraft, then GAMC. When NAA acquired GAMC, it consolidated three plants to one at Dundalk MD with approximately 150-200 employees remaining - then in turn was acquired by GM and divested of all commercial airlines save Eastern Airlines.
Summary, end of 1934.
All Teteboro Fokker/GAMC/Pittsburgh Aircraft aircraft had been completed, delivered, shut down.
American Pilgram 150/GAMC GA-43 completed at Dundalk as first actual NAA aircraft produced.
Berliner Joyce new development complete, only new orders for SOC-1 & -2 steel, welded floats are in production.
Senior management team execs Kindelberger (CEO), Atwood (Chief Engineering), Smithson (VP Production), Bowen (Production Engineer and future X73 project manager, then Asst Plant Manager at new Dallas Plant), Hansen (Chief Project Enginering) - ALL from Douglas Aircraft
Key Managers and future key employees Rice (Asst Chief, Engineering) - Douglas Aircraft, Schlecher (Chief, Airframe structures) and Baldwin (Project Engineer) and Rudd (tool & die maker who rose to VP&Gen Mgr NAA Columbus Div) came from Berliner Joyce. Schmued (Preliminary Design engineer at acquisition by NAA (GAMC)
Summary-
Every design produced by NAA from XO-47 (GA-15) and BT-9 (NA-16) through XB-21, BC-1, Export Fighter NA-44, AT-6, NA-40, B-25, P-51 were led by Atwood through 1939, Rice thereafter. Douglas origins.
Schmued became Chief, Preliminary Design in 1939 wth first effort the P-509/X73. The project team was matrixed but still in Rice's Engineering department.
The Production quality was driven by Kindelberger with focus on speed, quality and ever decreasing Cost. Smithson and imbedded project engineers worked closely with Design with an eye towards actual process, and process flow.
Schmued's genius were two fold. A superb intuitive feel for aerodynamic shape and ability to pick/lead and manage a preliminary design team to a schedule the preliminary designs.
Schmued also the driver for the development and implementation of Projective Geometry of applied conical sections. He pushed, Roy Liming constructed the application to the Lofting developments.
Additional Oddities
Nothing from Fokker related to manufacturing excellence, specifically not 'butt joint quality production that Greg cites as reason speed advantage over Spitfire. Curiously he didn't mention wing or Meredith effect as 'other reasons' for performance but all those lay at feet of Smithson, and Rudd including flush rivet passion and development of 7075 skin deelopment and techniques later. Nothing from Fokker instituted filling, sealing, priming and painting wing to achieve surface quality independent of butt joint construction.
Nothing from Fokker instructed Ed horkey, Ashkenas, Beerer (all Cal Tech grads) in the fine art of airfoil development, aerodynamics, performance analyss or Meredith effect cooling system design - the latter a far larger difference maker than butt joint construction.
Nothing from Fokker introduced alclad sheet stress panel analysis and design that was cornerstone of NAA quality and strength.
Greg cites Van Breese as one of the Fokker trained giants that vaulted the Mustang into glory?
Well, interesting that Van Breesehad his own aircraft company 1927-1934. Breese Aircraft Company. last operating at Mines Field. He co-designed the Vultee V-1. Was bought out during the Vultee consilidation. He DID consult with Fokker Netherlands as a Demonstrator test pilot for Various Fokker designs attempting to gain a foothold in 1937. From that approximate time he was basically a full time test pilot and consultant including a stint with NAA in 1939/40 for the NA-44 and then 73X
Now for the other side of the ledger.
The rapidity and excellence of the first big success of NAA Design - the NA-16 BT-9 - had a large contingent of Dutch speaking shop team that worked 18x7 to get the prototpe done in time to win against Seversky. While the GA-43 was largely GAMC (Pilgrim) workers, the BT-9 was welded steel tube fuselage and fabric covering for fuselage and wing - right in the strike zone for the surviving Fokker (and Berliner Joyce) cadre that made the trip to Dundalk.
If anyone feels like stirring up some stuff in Greg's new video, you have my permssion to cut and paste. Warning - you may get banned.
Sincerely,
Butthurt
I have it also as well as the Master Lines Manual, c/o Bob Boulier -prepared by Robert Curt Weebe. Apparently Weebe was dispatched from Inglewood to Dallas to not only serve as head of Lofting and Master lines but also teach at local UT classes - he retired as Group Leader back at Inglewood in 1966.I`ve got limings book on mathematics for computer graphics, inside are the programs to do the lofting of sections. Its quite a book.
It was not just Lindberg. He may have leaned out the engines a bit more but the British, Allison and Lockheed (and others) all used or recommended the low RPM and high boost method. British were using for both bombers and fighters ( Spitfire Vs with single stage superchargers) at least in 1942 if not before. As mentioned Lockheed test pilot Tony Levier gave demonstrations in Europe in the Spring of 1944 on several things concerning the P-38. Newsletters/updates from both Allison and Lockheed used the Low RPM and high boost method. The USAAC didn't believe them. It was NOT the manufacturer/s.In all the debate, I have not seen any comments about the techniques that Lindberg used to greatly extend the range of the P38 in the Pacific. Could not those same techniques have been used to great effect with both the P38 and the P47 in Europe in 1943? As near as I can tell, his main technique was to use high MP and low RPM's. Everyone thought it would damage the engines but it turns out that the engines ran quite rich when used as directed by the manufacturer.
1. The 2nd tier fighters do not have the range. If you are flying low and fast most fighters burn up fuel at a very high rate. Even around 250-260mph at 3000ft is going to burn around 60 US gallons and hour (for plane without drop tank/s). and at 250mph at 3000ft you are providing target practice for the German small AA guns and fighters. Fighters that were doing low altitude work near the channel generally used max continuous (2600rpm and 39in for an Allison) but that burned up 90-100 gallons an hour. Shooting up flak batteries for the first 50-60 miles of the trip into France when it was 200-400 miles more into Germany wasn't going to make much difference. Allies knew were the flak batteries were near the coast and they just flew around them.Flak suppression. Was this not a thing? Or were there just far too few fighters to even attempt? I've never seen anything about strafing runs on flak guns. Were they too widely disbursed to be strafed? Were they too hard to sight from the air? Would it be possible to have flak suppression on the flak batteries actually engaged in a specific attack? Wouldn't the "second tier" level of fighters not suitable for escort duties (P39, P40) be perfect for this tasking?
P-38s were a scarce commodity in 1943. In 1942 they only exceed 150 planes per month twice and in 1943 they only exceeded 200 planes per month once before October. The last 3 months of the year saw over 300 a month in all three months.The P38. Why all the focus on the P47 with regard to escorting? I'm well aware of the .68M/dive flap thing. But they could still "be there." Their presence could provide some level of deterrent and protection to the bombers. And they had the range and altitude capability.
If you're into literature about such things and want either a hardcopy book or an E-book, check out "P-51B Mustang: North American's Bastard Stepchild That Saved the 8th Air Force" by Bill Marshall and Lowell Ford (Bill is a poster here under the handle drgondog). It goes into the politics of why the P-51s introduction and widespread use in the USAAF was initially held back, those who ultimately advocated for it (such as various 8th AF generals and Hap Arnold himself, as the Mustang basically became the epitome of the high performance long range fighter he wanted since at least 1940), and issues with the P-38 and P-47.Hello
This is my first post. I have recently read through the posts regarding Greg's videos in this and another thread
I would like to offer my thoughts on the ongoing controversy regarding the "bomber mafia," strategic bombing, and the range of the P-47. I am not an "expert" by a longshot but I do have a passing interest in these topics. I consider myself a "swing voter" in this debate.
To me, Greg makes some good points. He did not create idea of the "bomber mafia." It does seem that many of the top men in the USAAF were in fact bomber men, that the "bomber mafia" was real.
The idea of a flying fortress has always seemed faintly ridiculous to me. A .50 caliber machine gun, or even a pair of them, aimed by a man wearing all the necessary equipment to stay alive, in an airplane moving 150-200 mph, at a target moving at an oblique angle at 300+ mph, and getting any hits, well.... that seems remote. Given the relatively short range of the weapons involved, it seems that a gunner would only have a very short window of time in which to get any hits, perhaps only one or two seconds. However, other targets were in range. The requirement to have a tight formation seems to exponentially expand the likelihood that countless friendly fire incidents happened. The whole idea is, to repeat myself, ridiculous to me. Wouldn't huge fleets of Mosquitos and B-26s, escorted by fighters and flying at least 100 mph faster (perhaps faster) be much more effective?
IMO, the bomber men that ran the USAAF seem to have avoided any responsibility for sending tens of thousands of men to their death. They also seem to have not understood the rapid pace of technological advancement in aviation. In short, they underestimated the fighters. This explains why there was lots of problems implementing drop tanks in 1943. They should have been tested thoroughly and in use before the USA even entered the war. Why weren't they? The fact that the whole drop tank development was done under war time pressure tells me that the leaders didn't take it seriously, in short, it appears to me that Greg's claim is correct. Furthermore, why was P38 development set back ~2 years? Basically because of a crash following what was essentially a publicity stunt.
I have a host of other thoughts, many of them concerning tactics, which as near as I can tell hasn't been discussed much. Frankly, the debate has sometimes devolved into pilots arguing about data in performance charts, with little talk about how the equipment (aircraft) were actually used. I should like to offer the following tactical considerations:
In short, I think the bomber offensives in 1943 were a huge failure and I blame the leadership of the USAAF. Many things that could have been done were not done. I'm reminded of Chihaya Masatake's comment about his leaders after Midway, "It could not be said of them 'everything was done that was humanly possible.'"
- In all the debate, I have not seen any comments about the techniques that Lindberg used to greatly extend the range of the P38 in the Pacific. Could not those same techniques have been used to great effect with both the P38 and the P47 in Europe in 1943? As near as I can tell, his main technique was to use high MP and low RPM's. Everyone thought it would damage the engines but it turns out that the engines ran quite rich when used as directed by the manufacturer.
- How to actually escort bombers? There is an interesting video on YouTube whereby Jimmy Thach gives a dissertation on how to attack another airplane. I think he gives 8 different methods if memory serves. What is the counter-vailing method of preventing those 8 types of attacks? The escorting fighter would have to be in the proper position at the proper time, all the time. Without the use of AWACS, this would have to be done by eye. Given the distances involved, and the speeds, it seems unlikely that the escorts could consistently be in the right place at the right time. In The Pale Blue Sky, by Jack Novey (B17 waist gunner), he gives examples when a single, slashing attack by enemy fighters shot down significant numbers of bombers. Chasing the attackers after they have made a successful attack is a pyrrhic victory. Yet, still, the mere prescence of fighters might be helpful in repelling or delaying attacks by German fighters.
- Forming up. It seems that significant time and fuel were expended in arranging formations after takeoff. The USAAF was very imprecise at that time. In both Schweinfurt raids, it appears that the bombers were late and disorganized. That would greatly complicate the task of escorting them. In short, the equipment and procedures of the time did not allow the level of precision required for both the bombers and the escorting fighters to organize their formations and maximize their effectiveness. And such operations weren't practiced in peacetime because "the bomber will always get through."
- Let's assume Greg is all wrong. Let's say that the bomber mafia believed in fighter escorts with drop tanks. If so, why did they screw up the implementation so badly, and why was it implemented so late?
- I have to say it. In the submarine war in the Pacific, lack of aggressiveness on the part of many skippers caused their relief from command. Is it possible that some of the fighter pilots in 1942 and 43 did not yet fully appreciate the tenacity and capabilities of the foe? Surely, the Schweinfurt raids were eye-opening, no one brainwashed by the daylight bombing narrative expected that level of loss in the bombers until it happened. One would think that after they saw how many bombers were lost, the resolve of the fighter pilots may have been bucked up somewhat. The submarine captain lack of aggressiveness is not highly publicized or talked about much, but it is recognized (Silent Victory by Clay Blair). Could some level of this same type of problem have been experienced in the fighter community of 1943 before Schweinfurt? We all want to think of fighter pilots as heroes in white scarves, but the reality is that they wanted to stay alive also, they were human beings not supermen, and they knew the value of their training and of their equipment to fighting in the future.
- Flak suppression. Was this not a thing? Or were there just far too few fighters to even attempt? I've never seen anything about strafing runs on flak guns. Were they too widely disbursed to be strafed? Were they too hard to sight from the air? Would it be possible to have flak suppression on the flak batteries actually engaged in a specific attack? Wouldn't the "second tier" level of fighters not suitable for escort duties (P39, P40) be perfect for this tasking?
- The P38. Why all the focus on the P47 with regard to escorting? I'm well aware of the .68M/dive flap thing. But they could still "be there." Their presence could provide some level of deterrent and protection to the bombers. And they had the range and altitude capability.
I'll add just a few more thoughts. Implicit in the P51 range discussion is how much less fuel it used. Multiplied by hundreds of airplanes, this efficiency puts much less demand on the supply chain for fuel. And also, less dependence on drop tanks decreases pressure on the supply chain to supply thousands of these expendable pieces of kit. The expensive (two engines) P38 and the fuel guzzling P47 both put a lot of pressure on the supply chain. But in 1943, they were the only potential escorts available in any significant number and to say they were underutilized is insufficient criticism when 10's of thousands of bomber crew were dying. It doesn't matter that the P51 was a better escort in 1944. I'm interested in why the P47 and P38 weren't used more effectively in 1943, and why no one was ever called to account for it.
Granted, I can also ask "how early do you want Merlin P-51s?". NAA had prototype/preproduction planes flying in late 1942, and there were the Rolls Royce Mustang Xs from earlier in the year. But it took time to optimize and refine the aircraft. However, the biggest hold up seemed to be Packard getting the two-stage Merlins into production. Some of this was tooling, perhaps having to expand the factory, and a lot of it was making single stage Merlins for British and Canadian Lancasters, and Canadian and Australian Mosquitoes, as well as for some P-40s.
Even if that came to pass, I doubt it would have resulted in an earlier start to "Big Week" simply because the weather is foul ad there isnt much daylight in December January, it may have resulted in a higher proportion of P-51s being used. One thing thee allies did to improve range was to reduce the distance. RAF Leiston was scheduled to be an RAF fighter base but was handed over before completion to the USAAF. Construction started in Sept 1942, completed in Sept1943, the 358th Fighter Group arrived with P-47s on 29 Nov from Scotland where they had been training and commenced Ops in December. The 357th arrived with P-51s on 31st Jan in time to take part in "Big Week". Some of my body fluids vaporise when I read that no one cared and nothing was done. Below is just one small example (RAF Leiston) of what was done in the exact period that is routinely moaned about. It was designated US station 373.About two years ago I asked Bill ( drgondog ) his best estimate how much sooner the P-51B could have started ops with 8th AF. There were more than just a few stars that would have had to align right and a certain Colonel getting hit by a beer truck was mentioned but in the end, Bill estimated maybe late fall early winter 1943, about five months earlier than it did. I wish I could find the post as he laid it out fairly well, if I have time I'll try to find it.