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The performance data obtained at Rechlin (either for W.Nr. 14010 or 14011) gives a maximum speed at 12,000m of 660 kph for a G-1/R2. I've no idea to what the 700 kph refers.
Yea right buddy. The attitude You try to practice are apparently based on some internet pages - and they are also secondary not primary as you seem to think. Come back with Your attitude when you have a Phd thesis from a respectable institute on the subject. Until then, your info is no better than the one I referred to.
Comparing performance info from different sources makes little sense to me. Anyone who want to compare are better off using info from one source only (such as Rechlin for instance)
Fair enough but a well documented single source is a useful place to reference and begin the dialogue..
Carry on.
Attitude cuts both ways, does it not?
Vogt states the following production numbers for the G1:
Mtt R Werknr 14004-14070 67 (units) G-1
Mtt R 14071-14149 79 G-1/R2
Erla 10299-10318 20 G-1
So a grand total of 166 units of the G-1 model built.
The only weight stated by Vogt for a G-1 are for a G-1/R2 and he claims 2970kg. For that same model he also claims the climb rate to be 22m/s, the ceiling 12 600m and as mentioned 700km/h top speed.
OK - Nowarra cites G-1 empty weight as 2700 and 'all up weight' as 3150 with a useful load of 450kg. His tables have 623km/hr. What should we infer? Any useful data regarding altitudes for the data points presented, fuel load at altitude (therefore gross weight different from take off?). Nowarra has the equivalent table top speed for the F-4 at 635km/hr.
Might we infer that Vogt could have been mistaken to cite a G-1/R2 at 700km/hr top dash speed? The difference between Vogt and Nowarra would seem to be the R2 congig for gross weight - making the 700km/hr equally suspect.
On the thread subject of comparing different models, Vogt states the following performance numbers for an F-4. Top speed 670km/h,weight 2740kg, climb rate 17m/s and a ceiling of 11 800m.
What is your reference for that 660 km/h speed at 12000m? It seems highly unlikely that any 109 powered by a 605A engine would reach such a speed at high altitude without the use of nitrous or methanol.
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I never commanded anything from tomo. It was tomo that disrespected me by belitteling my reference to a secondary source and demanding authority for His claim because of his reference to a single internet source. Pretty low I think.
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that stirred me. If you want respect, not the best way to gain one. I've replied in a similar manner.And your sources are the internet references you made right?
Nothing wrong being curious. But, by the way what did You bring to the table to command anything?
Which table? Aerodynamics, Airframe Structures, Performance, Flight Mechanics, History, Finite element methods for pressure distribution, Finite element/relaxation methods for airframe Structural analsis? Pick one.
I confess I haven't written a Doctoral thesis, but I managed to bumble my way throught a MS Degree in Aerospace Engineering. My MS thesis was probably simple stuff for you but I'm open to criticism on "Effect of Geometry of a Rotor Centerbody Immersed in a Ducted Fan" - Univ Texas 1972. I used Complex variables to model source/sink distributions to drive both the flow through the system, changes to the geometry of the centerbody, and calculate the pressure distributions. How would you suggest that I should have done it?
I can't compete with the giants but I did pioneer finite element/relaxation methods for airframe structures on the SR-71 and the Bell 209/AH-G Iranian Cobra with NASTRAN and it was the first computer method accepted by the US Army. Not up to your standards, I'm sure but I did the very best my limited capacity enabled me to achieve... and you?
I never commanded anything from tomo. It was tomo that disrespected me by belitteling my reference to a secondary source and demanding authority for His claim because of his reference to a single internet source. Pretty low I think.
Tomo didn't belittle you. If you believe that, your 'feelers' are incredibly sensitive to any comment about your way of thinking below the level of worship or adulation. If that is what you seek here, your fragile ego will be crushed beyond recovery going forward.
Since when became a Internet reference a more valuable source than an physical book?
Well, trick question! But when they are one and the same there is no 'advantage' one way or the other. On the other hand you must compete with the largest and most accessible library and knowledge repository on the earth - with your single 'physical book'. Are you a world class sprinter or a one legged man in an ass kicking contest?
Is a pdf-scan of a certain paper published on a web-page more valuable than publishing the same piece of information and picture in a book?
See above for clarification. Read two or more times for comprehension?
Do you guys have a specific standard for making statements about old airplanes?
Just curious...
It all depends on the book, too many lousy books in the market or those replicating way outdated information. Then we have books that just use other books as reference, copying also the errors of these books.Since when became a Internet reference a more valuable source than an physical book?
Is a pdf-scan of a certain paper published on a web-page more valuable than publishing the same piece of information and picture in a book?
Do you guys have a specific standard for making statements about old airplanes?
Just curious...
Yea right buddy. The attitude You try to practice are apparently based on some internet pages - and they are also secondary not primary as you seem to think. Come back with Your attitude when you have a Phd thesis from a respectable institute on the subject. Until then, your info is no better than the one I referred to.
Comparing performance info from different sources makes little sense to me. Anyone who want to compare are better off using info from one source only (such as Rechlin for instance)
Carry on.
Yes the G1 had a pressurized cockpit and the G2 did not, but more important was the G1 was stripped down in weight compared to the G2.
It is not clear if nitrous injection (GM-1) was a standard for any 109 model type. What is clear is that it was an Umrustsatz (U2) available. For the G5 model type it is possible that all were factory built with the U2 and that would make an argument for the G5 as being standard equiped with nitrous.
I am not an expert in this area but if the G1 had the Pressurised cockpit and the G2 didn't, but the G1 was weighed less, how can they be basically the same aircraft?
The 640 km/h for the G-2 is impossible with fully rated engine, even the heavier and bulkier G-6 achieved ~645km/h as max. This G-2 speed is obviously with derated engine.
The Bf 109G typically achieved its max speed roughly 500m above the rated alt of the engine.
~625 km/h is the typical max speed for Bf 109 G-6 at climb&combat power rating.
The 700 km/h are a bit irritating indeed, could only be the weight-saving G-1 version or a G-1 with GM-1.
Yes, I would agree that 640km/h for the G2 seems low for full boost (1.42ata). That speed seem more likely for 1.3ata boost (maybe that is what you mean with derated?).
As pointed out by others above , many different sources stated max speed for the G-1 to around 650-662km/h. According to the information on the Kurfürst-site (that many apparently think highly of here) the speed of 660km/h was with the lower boost of 1.3ata (stieg und kampfleistung) To me, it is obvious that max speed of the G-1 at the higher 1.42ata boost would be higher. Then was it actually 700km/h? The question has to be adressed and answered by the source I gave (Vogt). His book is almost brand new so it is fair to assume that he had access to all of the other sources that has been mentioned in this thread.
By the way, I do not consider wikipedia as a reliable source but I must point out that the same figure, 700km/h for the G-1 is stated there FWIW...
The first G-1s,including a couple of the lightened ones,went to Rechlin in March 1942 for testing. Despite the many problems encountered they were soon (May?) sent to the Channel front.
JG 2 and JG 26 both had some. They were supposed to enable interception of the RAF's high altitude bombers and reconnaissance aircraft,presumably meaning PR Spitfires and of course Mosquitos which were appearing around this time and obsessed the Luftwaffe for the rest of the war.
They were also used as high altitude protection for the Fw 190s whose BMW 801 engines did not perform well at altitude.
JG 1 (I think then in Holland) and JG 5 in Norway also received the type early on.
Cheers
Steve