Why no Fw 190H but the Ta 152H? (2 Viewers)

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Look at the image I posted in the previous image - the Ta 152H used a NACA 230xx airfoil at the root. The NACA 5-digit airfoils have very little laminar flow.

Hi,

Thanks for that original data page. The Ta 152 H-1 profile seems to indicate both "NACA 230" and Fw in the box, which is different to all the other types shown. Given the very different detail of the 152 H high aspect ratio wing, is it not likely that this shows a root area NACA 230 profile, developing into an unspecified Fw profile in the very different outer sections?

Cheers

Eng
 
From "The Focke Wulf Ta 152" by Hitchcock:
"Steel had long been planned for both the Fw 190 and the Ta 152; specifically for use in the wing spars and skinning despite a 15 to 25 percent weight penalty. "
Since the paragraph it is taken from is a discussion of the wing design I presume it is 15 to 25 percent of the total wing weight, not the entire aircraft.
250 kg would equate to a wing weight of 1000 to 1700 kg. I can't find any info on the wing weights but it doesn't seem reasonable to me.

"Focke Wulf Ta 152" by Dieter Harmann gives a breakdown of weights for the Ta 152 H-0 and H-1.
I was interrupted before I could give the weights . Here they are
1766432733403.png

I used goggle translate for the English names so please correct as needed.
 
I used goggle translate for the English names so please correct as needed.
'Tragwerke' - 'Lifting device' - wing.
The term 'Triebwerke in der Zelle' - Powerplant parts in the airframe' are the fuel tanks and ancillaries to the fuel system, like pumps, lines, controls, valves etc.
'Triebwerke vor the Brandschott' - 'Powerplant in front of the firewall' includes everything in front of the firewall (but not the guns, for example) - engine, engine bearer, cowling, prop, as well as the cooling system etc. Fw 190s and it's cousins were no jokes in this regard :)
 

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