buffnut453
Captain
Expert
/ˈekˌspərt/
noun
Person from out of town with a brief case
Ex-spurt....Ex as in has-been, spurt as in drip under pressure
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Expert
/ˈekˌspərt/
noun
Person from out of town with a brief case
Height ft. | T.A.S. m.p.h. | Time From Start Min. | Rate of Climb Ft./Min. |
2,000 | | .7 | 2,820 |
5,000 | | 1.8 | 2,850 |
10,000 | 320 | 3.5 | 2,895 |
11,000 | | 3.9 | 2,905 |
15,000 | 339 | 5.4 | 2,430 |
18,900 | 354 | | |
20,000 | 353.5 | 7.7 | 1,840 |
25,000 | 345 | 11.0 | 1,250 |
30,000 | 319 | 16.4 | 660 |
Height Feet | Top Speed M.P.H. | Time To Climb Mins. | Rate of Climb Ft./Min. |
S.L. | 290 | - | . |
2,000 | 294 | 0.7 | 2925 |
5,000 | 306 | 1.7 | 2955 |
10,000 | 326 | 3.4 | 2995 |
15,000 | 345 | 5.0 | 2770 |
20,000 | 351 | 7.0 | 2175 |
25,000 | 338 | 9.6 | 1600 |
30,000 | 321 | 13.7 | 995 |
I just called it a faked test report and someone got upset. 3 consecutive figures of 3,720 for rate of climb exactly the same mean thrust, lift drag remained almost the same from SL to 10,000ft the difference exactly compensated for the loss of fuel and oil burned. Or it was faked. estimated or averaged out.That's unusual!
The Spitfire I has exactly the same time to climb as that stated for the P-39C to 25,000ft, despite the Spit. being considerably lighter, with more wing span and wing area. It isnt impossible but needs special aerodynamics to produce more lift with less drag.So we have the lightweight, non-combat capable P-39C that, in early 1941, can reach 30,000ft in 18.4 mins and has an absolute ceiling of 34,150ft.
For comparison, here's a Spitfire MkI trial from 19 March 1940 showing performance with a constant speed Rotol propellor (source: Spitfire Mk I Performance Testing)
Height
ft. T.A.S.
m.p.h. Time
From
Start
Min. Rate
of
Climb
Ft./Min. 2,000 .7 2,820 5,000 1.8 2,850 10,000 320 3.5 2,895 11,000 3.9 2,905 15,000 339 5.4 2,430 18,900 354 20,000 353.5 7.7 1,840 25,000 345 11.0 1,250 30,000 319 16.4 660
Service ceiling = 34,700 ft.
And we're supposed to believe that taking some guns and 100lb out of the P-400 or P-39D is going to "improve performance tremendously" when the lightweight P-39C was bested by an aircraft that was operational a year before it?
I think you'll find that steel was used in many high stressed areas on several combat aircraft of the period. In later years 7075 forgings or titanium would be used in these applications but you still might find steel depending on the type of aircraft and manufacturer.Note the use of steel.
View attachment 631725
The Spitfire always had steel wing spars and was always a light design, the Blenheim used steel box work in its structure and was always a deceptively heavy light bomber. Ingenuity counted for a lot at the time.I think you'll find that steel was used in many high stressed areas on several combat aircraft of the period. In later years 7075 forgings or titanium would be used in these applications but you still might find steel depending on the type of aircraft and manufacturer.
This graph is a projection, not actual. Dates on graph predate production. I'm referring to the July 1941 P-39C Wright Field test.That's an interesting graph...but I have huge questions over its accuracy. It claims that the P-39C had a ceiling of approx 37,500 ft and can reach 30,000ft in less than 12 minutes. However, the tabular data on this page (P-39 Performance Tests) lists the absolute ceiling for the P-39C as 34,150ft and time to 30K in 18.4 mins. These figures seem much more realistic than the chart MIlosh posted...but why the discrepancy since both were apparently created by Wright Field test pilots?
The performance characteristics for the P-39D-1 listed in this table:
The P-39D-1 can't reach 31,000ft as a service ceiling and takes 25.7 minutes to get there. Even the later N and Q models take more than 25 mins to reach service ceiling.
Radio: AHT listed the voice radio in empty weight, IFF radio as part of load. What else would it be?AHT says in the table.
"Misc. equip (radio)"
If it says IFF somewhere else please point it out.
The radio was included in the empty weight of the P-39C as per the Manual.
It was NOT included in the empty weight of the P-39D-1 and P-39D-2 as per the manual.
By the time you get to the P-39N the radios (included is the IFF) are back to being in the empty weight. They are the same radios as used in the P-39Ds. They are listed by type/model number. This probably one of the reasons the P-39N was about 100lbs heavier empty than the P-39D?
Make sure you are comparing like to like.
So you used a WAG to come up with your number.
You could have just used the armament provision number for the P-39D-2
Funny thing about that.
In the Manual for the P-39C the performance number page (page 22) says the level speeds were with a design gross weight of 662lbs. an obvious typo.
The climb data (IAS as various altitudes, no climb rate given) was for a design gross weight of 6662lbs.
The landing and take-off distances are given for a design weight of 6662lbs.
the weight chart comes up with a weight of 6684lbs with 104 gallons of fuel. There are no self sealing tank liners or tanks. full fuel is 170 gallons.
Things change with time. This was common practice in the late 30s or 1940 (?)
The P-36 and early P-40 performance specifications also use a limited fuel load. The performance numbers are done with 105 gallons in the case of the P-36 with a 57 gallon overload tank available
see http://www.wwiiaircraftperformance.org/P-36/P-36_Operation_and_Flight_Instruction.pdf
The P-40 numbers are really strange.
see; http://www.wwiiaircraftperformance.org/P-40/P-40_Official_Summary_of_Characteristics.pdf
normal fuel is 120 gallons, max is 181 gallons.
Performance numbers are for 120 gallons. at a design weight of 6787lbs
So, in this case the P-39C was tested at about 27lbs over it's "design" gross weight. Which is close enough, maybe they couldn't find a test pilot that weighed 160lbs in flight suit and with parachute.
If it is you are going to run out of oil before you run out of gas. P-39N carried 62lbs of oil including the gear box oil for it's 87 gallons of fuel. The P-39Ds carried 88lbs of oil including the gear box oil, Both could and did carry more oil when the drop tank was fitted. The P-39C carried 7.4 gallons in the main tank/engine (55lbs) with 15lbs for the gear box on a separate line. The tank could hold 12.1 gallons. Again the "normal" fuel load for the P-39C was 104 gallons.
Perhaps planes in combat zones carried an extra gallon or two just for "insurance"?
I know I would try to, especially if the engine was somewhat worn.
Apparently the P-39C had semi automatic cooling flaps. At high speed the airflow pushed them shut.
There is also a difference between a plane that has trouble cooling in a long hard climb and one that overheats in high speed level flight.
What is your point about all this? Arguing about the weight of every component, presenting and representing discredited tests. It has been going round and around for years.Radio: AHT listed the voice radio in empty weight, IFF radio as part of load. What else would it be?
Yes WAG for 30cal portion of "Armament Provisions". Please provide a more accurate WAG.
Average American man in the Army in WWII was 5'8" and weighed 140lbs. Fast food hadn't been invented yet.
What is your point about the amount of oil?
No auto cooling flaps. Spring loaded, airstream pushed them back partly closed.
Are you saying that the P-400 weights I furnished are not correct?
What is your point about all this?
It would have been if gravity and the British hadnt got involved in an unholy conspiracy.That the P-39 was the F-22 of its day? Something like that, it seems.
Where in AHT does it say that?Radio: AHT listed the voice radio in empty weight, IFF radio as part of load. What else would it be?
Great, naked pilot with 20lb parachute.Average American man in the Army in WWII was 5'8" and weighed 140lbs. Fast food hadn't been invented yet.
Point is you have to use the right weight for the mission, not the weight that looks the best.What is your point in British about the amount of oil?
Couldn't ball turret gunners be re trained to fly P-39s? I am trying to think outside the box.With clothing and gear W&B in the Form 1 was calculated at either 180 or 200 pounds
View attachment 631745
View attachment 631746
View attachment 631747
Even the stuff about radios I dont get, the British had been using radios in planes since around 1930.
I didnt know when they switched from Morse to voice.Actually since 1918. There was operational use of radios for air-to-ground communication in 1918 by 11 Sqn RAF.
You jest? Bomber command aircraft carried pigeons throughout most of the war (until 1943) Carrier Pigeons in the Bomber WarThey tried carrier pigeons but they kept getting hit by the tail surfaces when released.
My coat is nearby.