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delcyros said:A problem for the P-39 was the comparably heavy weight. The VVS usually removed cockpit armor and took on further weight saving measures, from which the airplane benefitted, esspeccially at low alt.
FLYBOYJ said:Yep - When the P-38 started experiencing compressibility problems Wright Patterson engineers tried to put their 2 cents in. One recommendation was the installation of the elevator mass balance commonly seen on the P-38s tail. I attended a Lockheed Management club dinner back in 1982 and Kelly Johnson was the guest speaker. He said the mass balance does nothing and he agreed to install them just to shut up the AF engineers!
wmaxt said:FLYBOYJ said:Yep - When the P-38 started experiencing compressibility problems Wright Patterson engineers tried to put their 2 cents in. One recommendation was the installation of the elevator mass balance commonly seen on the P-38s tail. I attended a Lockheed Management club dinner back in 1982 and Kelly Johnson was the guest speaker. He said the mass balance does nothing and he agreed to install them just to shut up the AF engineers!
Not just to shut them up - the AAF threatened to stop the contract as they were convinced that was the cause of the tail buffet, compressability showed up at the same time but was a different issue. The introduction of the root fillets at the wing/gondola juncture smothing the airflow fixing the buffet. Incidentaly the roll down side windows did the same thing when they were opened.
wmaxt
FLYBOYJ said:delcyros said:A problem for the P-39 was the comparably heavy weight. The VVS usually removed cockpit armor and took on further weight saving measures, from which the airplane benefitted, esspeccially at low alt.
Did they removed all the armor?
DerAdlerIstGelandet said:I hope they removed more than just the cockpit armor. That would mess up the CG of the aircraft!
JamesBlonde said:Removing a bit of armour shouldn'y make much difference.
FLYBOYJ said:JamesBlonde said:Removing a bit of armour shouldn'y make much difference.
I hate to say it James but that is wrong. As little of 5 pounds removed or added can shift the center of gravity out of limits. If the aircraft gives little or no stall warning, this could be disastrous during landing and especially if a green pilot is flying.
This is 4x more critical on helicopters, just ask Adler!
wmaxt said:You have to take into consideration where in relation to the CG the weight is. 5 pounds in the tail is may affect the CG more than 100lbs 1 foot aft of the CG.
In the P-39 the armor was very close to the CG and made little if any difference in it. Modified P-39s were very fast, after the war they won many air races. Speeds comparable to P-38s anf F2Gs and normaly faster than the P-51s until the more modified P-51s started showing up.
In the hands of a good pilot it was pretty effective and quite maneuverable, though it had been hurt badly by the Engineers at Wright Patterson AB with "It looks Good" engineering. When used in a way that matched it's capabilities it was an effective aircraft!
wmaxt
FLYBOYJ said:wmaxt said:You have to take into consideration where in relation to the CG the weight is. 5 pounds in the tail is may affect the CG more than 100lbs 1 foot aft of the CG.
In the P-39 the armor was very close to the CG and made little if any difference in it. Modified P-39s were very fast, after the war they won many air races. Speeds comparable to P-38s anf F2Gs and normaly faster than the P-51s until the more modified P-51s started showing up.
In the hands of a good pilot it was pretty effective and quite maneuverable, though it had been hurt badly by the Engineers at Wright Patterson AB with "It looks Good" engineering. When used in a way that matched it's capabilities it was an effective aircraft!
wmaxt
I agree for the most part however even with the armor close to the CG, I believe the CG envelope of the 39 was only a few inches. Removing the armor and flying the aircraft full of fuel or with minimal fuel could produce undesirable results. I would like to get my hands on a P-39 W&B chart and find out how much armor was actually carried on the -39....
The post war 39s and 63s were very fast and when they were modified, and I'm sure that when armor and guns were removed, in some cases ballast had to be added as well.
FLYBOYJ said:I agree for the most part however even with the armor close to the CG, I believe the CG envelope of the 39 was only a few inches. Removing the armor and flying the aircraft full of fuel or with minimal fuel could produce undesirable results. I would like to get my hands on a P-39 W&B chart and find out how much armor was actually carried on the -39....
The post war 39s and 63s were very fast and when they were modified, and I'm sure that when armor and guns were removed, in some cases ballast had to be added as well.
wmaxt said:FLYBOYJ said:I agree for the most part however even with the armor close to the CG, I believe the CG envelope of the 39 was only a few inches. Removing the armor and flying the aircraft full of fuel or with minimal fuel could produce undesirable results. I would like to get my hands on a P-39 W&B chart and find out how much armor was actually carried on the -39....
The post war 39s and 63s were very fast and when they were modified, and I'm sure that when armor and guns were removed, in some cases ballast had to be added as well.
The weight and Balance sheet and the armor location/weight charts would tell us if ballast was required.
The P-39 though didn't have issues like the P-51 where the fusalage tank could actually go from one extreme to the other. I've just never heard of serious problems with the P-39 regarding CG issues. Removing the armor was common on P-39s.
wmaxt
FLYBOYJ said:And I could tell you in "basic pilot 101" reward CG is not a good thing, especially for newer pilots. I also found data that the Russians issued directive to P-39 pilots not to pull out of dives in a left turn...the tail could be pulled off!