Oberst_Emann wrote:
Could you also kindly explain to me how the 262's wings were "conventional"?
1) could you kindly explain to me how they were NOT conventional?
2) the 262 had serious compressibility problems at high Mach number, due to its thick-profile
conventional wing. Further upgraded versions (HG etc.), which AFAIK never flew, had a new, thin-profile,
advanced laminar-flow wing. Aircraft aficionados will probably recall the similar evolution from the thick-profile
conventional wing of the Typhoon to the thin-profile
advanced wing of the Tempest. This was a
big technical step, although it is not readily apparent.
3) only these HG evolutions would have a
truly swept-back wing. Although some people call the 262 a swept-back wing plane, they have probably never realized how the 262 wing shape looks like the C-47 wing shape. Surely they will not call the Dakota a swept-wing plane, will they?
4) additionally, HGs will at last have its engines placed in a clever position, rationally designed to minimize drag.
Do you want to see an
advanced, rationally-designed, German jet planes? Look at Ta 183 (which heavily influenced MiG-15).
http://www.luft46.com/fw/ta183-i.html
Davide