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And it conflicts with part of the flight manual - Depending on how you fly its off by 6 gallons. This is about climb, not miles flown. Do you know what Vx and Vy is???The 20gal on the Flight Operations Instruction Chart is correct. It is an allowance. And it assumes climb to higher altitude starts at 5000' having traveled zero miles. This is being conservative since at least as soon as gear/flaps are up and climb speed is attained after form up the pilot will vector toward target. Then another 4.5min climbing to 5000' toward the target means an extra 13mi not included in calculations.
Again at what rate of climb?? What RPM??? VX or VY???? Those AAF offices were smart for the most part but got a lot wrong that has been clearly pointed outYes fuel will be burned climbing from 5000' to 25000' but 73mi range will be gained by climbing at 170mphIAS (220mphTAS average) for 20minutes in the direction of the target. One more time, this has all been factored into the range calculations for every altitude and every power setting. Take any amount of fuel available at any altitude at any power setting (RPM/manifold pressure) and do the math. Available fuel divided by gallons per hour x TAS is always more than the range figure quoted. The very smart AAF officers who put together these charts accounted for the fuel burned/miles gained by climbing from 5000' to whatever altitude is chosen. They did this to lessen pilot workload and get all the range information on one chart. You don't need the Takeoff, Climb and Landing Chart for any range calculations.
You hear WRONG. 30 minutes is normal, 45 for IFR, the navy used 60. Did yo hear that from a gaming site?But I thought that previously you couldn't find any mention of any reserve for landing anywhere. Now we need 30minutes (you would use 45) to find our home field. That hasn't moved. I have always heard that the AAF used 20min.
I'm not the one who has made outrageous claims on here and been proven wrong by a host of people on this forum with years of aviation experience.Or maybe you have been in your pixie dust, unicorn poop or mystical incantations again. I just use the appropriate flight manual.
No kidding! I never knew that! How many mag checks have you done????Yes, the P-38 was a twin meaning that two engines must be started (separately) and two sets of propeller and mag checks must be undertaken (separately).
Why dont you show us some math! On ram pressure, superchargers, compression and combustion, flame fronts mean effective pressure, propeller efficiency, lift drag. You could also try to explain how a plane becomes more economical as it gets closer to dropping out of the sky?Take any amount of fuel available at any altitude at any power setting (RPM/manifold pressure) and do the math.
Thats worth 400 miles of fuel in a P-39. No wonder the P-38 wasnt produced much.Yes, the P-38 was a twin meaning that two engines must be started (separately) and two sets of propeller and mag checks must be undertaken (separately).
You don't need the Takeoff, Climb and Landing Chart for any range calculations.
P-39 Expert said:Or maybe you have been in your pixie dust, unicorn poop or mystical incantations again. I just use the appropriate flight manual.
No conflict, the 20gal is an allowance on the range chart. It ties into the rest of the numbers on the chart. The 26gal is a measurement on the takeoff, climb and landing chart. It has nothing to do with computing range. Everything you need for computing range is on the range chart.And it conflicts with part of the flight manual - Depending on how you fly its off my 6 gallons. This is about climb, not miles flown. Do you know what Vx and Vy is???
I clearly pointed out that climb speed for the P-39N was 170mphIAS. The average altitude between 5000' and 25000' is 15000'. 170mphIAS at 15000' is 220mphTAS. I said all of that.Again at what rate of climb?? What RMP??? VX or VY???? Those AAF offices were smart for the most part but got a lot wrong that has been clearly pointed out
I was wrong? A few pages ago you had never heard of a landing reserve and couldn't find it quoted anywhere. I was the one that told you the USN used a 60min reserve to find an aircraft carrier maneuvering in the open ocean. Now you are the expert on landing reserve?You hear WRONG. 30 minutes is normal, 45 for IFR, the navy used 60. Did yo hear that from a gaming site?
There's a host if items that I have been proven correct. You have not proven me wrong on this range chart subject yet and I suspect that you won't.I'm not the one who has made outrageous claims on here and been proven wrong by a host of people on this forum with years of aviation experience.
I'm not a pilot but I have read the pilot manuals. If you have to be correct on every subject just because you are a pilot then the rest of us should just give up? Bill can compute his own crazy flight plan. I have computed numerous flight plans on here for the P-39 and the P-47 and the information comes straight from the manuals. Poor Buffnut. He's so concerned about the type of cabin heat on the P-39C when only 20 examples were completed and none saw combat. 20 examples. And I have explained on more than one occasion which models had the gas heater and which models had ducted air heat.When are you going to do Bill's flight plan? When are you going to show us actually flight planning you have done? When are you going to show up your aviation resume? When are you going to answer poor Buffnut!
I have shown you the math on every single example. The available fuel, altitude, gallons per hour and IAS/TAS are straight from the manuals.Why dont you show us some math! On ram pressure, superchargers, compression and combustion, flame fronts mean effective pressure, propeller efficiency, lift drag. You could also try to explain how a plane becomes more economical as it gets closer to dropping out of the sky?
All you do is take numbers from a manual that are guidelines or wrong and multiply or divide them.
Poor Buffnut. He's so concerned about the type of cabin heat on the P-39C when only 20 examples were completed and none saw combat. 20 examples. And I have explained on more than one occasion which models had the gas heater and which models had ducted air heat.
So you maintain that fuel economy increases with speed and altitude? Regardless of how many thousand feet you are above rated altitude and that the most economical altitude is where max speed, stall speed and cruise are the same? Have you any figures let alone a manual number for a P-39 at 30,000ft after dropping a 110gal tank at 25,000ft and climbing there? It is a fantasy nonsense scenario that defies physics, flight tests, everything I have ever read about flight and my whole life experience working with engines from mopeds through racing bikes to 5 litre V8s going across Saudi Arabia.I have shown you the math on every single example. The available fuel, altitude, gallons per hour and IAS/TAS are straight from the manuals.
I have shown you the math on every single example. The available fuel, altitude, gallons per hour and IAS/TAS are straight from the manuals.
This is pure gold...I'm not a pilot but I have read the pilot manuals
This is pure gold...
When are you going to do Bill's flight plan? When are you going to show us actually flight planning you have done? When are you going to show up your aviation resume? When are you going to answer poor Buffnut!
Did the gas heater have weight? Yes. Was it necessary? No. Did the British order it on the P-400? Yes. Was it on any P-39 model not produced for export? No. Except the P-39C of which only 20 examples were produced. Gas heater on export models P-400, P-39D1 and P-39D2. No gas heater for domestic models P-39D/F/K/L/M/N/Q. Is this clear enough? Am I dodging your question in any way? This is about the 4th time I have explained this to you.No you haven't explained. You keep stating that the export models had the gas heater while D variants onwards had ducted air. The number of P-39Cs produced is entirely irrelevant. It's simply a fact that it was a production airframe. I suspect that you keep equivocating on the topic because you clearly understand the thrust of my argument. You keep asserting that the dastardly Brits specified the unnecessary gas heater in a deliberate attempt to increase the weight of the P-400. The key flaw in this entire ridiculous argument is the timing of these events.
The British ordered the P-400 in late-1940. That was before the P-39C's first flight. Since the C variant also had the gas heater, it makes perfect sense that the same installation would be offered to the British as standard equipment for the type.
Furthermore, in order for the British to specify an extra and superfluous gas heater in late 1940 to deliberately make the P-400 overweight, it would mean they were attempting to sabotage the entire programme before any production P-39 variant had flown. Aside from requiring some real crystal ball gazing, why didn't they just not order the damn things and be done with it? Why go through the pain of deliberately ordering too much equipment on an aircraft that they'd already decided was useless before it was flown? That makes absolutely ZERO sense.
I really couldn't give two hoots about the various heaters in the P-39 variants. I do object when people trot out complete bullshit and refuse to acknowledge any evidence that contradicts it.
Looking forward to hearing how you try and dodge out of this latest information that flies in the face of your conspiracy theory.
Bell told the British that this BS aeroplane had a ceiling of 36,000ft so it needs a heater for the pilot and the guns, as you have been told NAA put the same heater in the Mustang I without protest for the same reason. BTW the USA wasnt at war at the time, was it?Did the gas heater have weight? Yes. Was it necessary? No. Did the British order it on the P-400? Yes. Was it on any P-39 model not produced for export? No. Except the P-39C of which only 20 examples were produced. Gas heater on export models P-400, P-39D1 and P-39D2. No gas heater for domestic models P-39D/F/K/L/M/N/Q. Is this clear enough? Am I dodging your question in any way? This is about the 4th time I have explained this to you.
Did the gas heater have weight? Yes. Was it necessary? No. Did the British order it on the P-400? Yes. Was it on any P-39 model not produced for export? No. Except the P-39C of which only 20 examples were produced. Gas heater on export models P-400, P-39D1 and P-39D2. No gas heater for domestic models P-39D/F/K/L/M/N/Q. Is this clear enough? Am I dodging your question in any way? This is about the 4th time I have explained this to you.
Bell told the British that this BS aeroplane had a ceiling of 36,000ft so it needs a heater for the pilot and the guns, as you have been told NAA put the same heater in the Mustang I without protest for the same reason. BTW the USA wasnt at war at the time, was it?
Bell didnt do anything to tell the RAF that their estimates were way off. Supermarine almost lost the contract for Spitfires because of low levels of production between 1936 and 38, a part of this was the difficulty of producing wings, but within that as soon as the first models were tested the wings had to be changed to incorporate ducted heating. If the guns dont work the aeroplane is FFFing useless, a danger to its pilot and everyone that depends on it up to Churchill himself. I cant accept this being treated as a petty issue by the expert, it wasnt, and no requirement was placed on Bell that wasnt placed on everyone else. In fact I would go as far as saying gun heating on USA aircraft was something learned by the USA from British or others specifications, Bell were just behind the curve as usual.I think your first point there is the crux of the matter. The Brits ordered the P-400 before any operational variant P-39 had flown. We have no idea what performance claims were made by Bell, although the chart provided earlier in this thread gives some indication that the pre-1941 performance estimates were ridiculously optimistic. Rather than the Brits deliberately besmirching the good name of Bell, it seems far more likely that Bell sold the Brits a bill of goods....and then failed to deliver on it.
YES IT IS A CONFLICT!No conflict, the 20gal is an allowance on the range chart. It ties into the rest of the numbers on the chart. The 26gal is a measurement on the takeoff, climb and landing chart. It has nothing to do with computing range. Everything you need for computing range is on the range chart.
OK ... and???I clearly pointed out that climb speed for the P-39N was 170mphIAS. The average altitude between 5000' and 25000' is 15000'. 170mphIAS at 15000' is 220mphTAS. I said all of that.
The reserve you are attempting to explain is an extended flight reserve just in case you get lost or have to deviate. It is there to make it to your destination. Again, your terminology as a novice further shows your lack of understanding. And yes I AM AN EXPERT ON FLYING WITH A FUEL RESERVE! I'VE DONE IT! HAVE YOU????I was wrong? A few pages ago you had never heard of a landing reserve and couldn't find it quoted anywhere. I was the one that told you the USN used a 60min reserve to find an aircraft carrier maneuvering in the open ocean. Now you are the expert on landing reserve?
I have but you're too much of a narcissist to admit when you're wrong, not only to me but to many other members on this forum!There's a host if items that I have been proven correct. You have not proven me wrong on this range chart subject yet and I suspect that you won't.
We can definitely see that! I guess I can read manuals about brain surgery too!I'm not a pilot but I have read the pilot manuals.
Rest of "us"?? No, but maybe YOU should! I think it's "YOU" vs. "the rest of us!" There have been many well versed members on this forum who have proven me wrong many times (some of them "non-pilots") and when I see the evidence in front of me I take it as a learning experience, something that I've made a point to do when I first started in aviation over 40 years ago, but I think it's almost comical when you have 5 or 6 members coming up with the same conclusions who actually flown aircraft or worked in the industry attempting to show you the errors in your ways and you refuse to listen! But then again, you're NOT a pilot but read the manuals!If you have to be correct on every subject just because you are a pilot then the rest of us should just give up?
And probably half of what you're computed is in error because despite "reading the manuals" you don't have the training or background to fully grasp what you're looking at!Bill can compute his own crazy flight plan. I have computed numerous flight plans on here for the P-39 and the P-47 and the information comes straight from the manuals.
First time I'm hearing it!Poor Buffnut. He's so concerned about the type of cabin heat on the P-39C when only 20 examples were completed and none saw combat. 20 examples. And I have explained on more than one occasion which models had the gas heater and which models had ducted air heat.