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433. oldal
The wing section was R.A.F.69 . To make the machine more manœuvrable , the washout was reduced to 8 ° at the tips . Built as a pure cantilever , we estimated that the wing would 32 ° and ASTRONAUTICS aircraft , with the exception of the ...
The wing section was R.A.F.69 . To make the machine more manœuvrable , the washout was reduced to 8 ° at the tips . Built as a pure cantilever , we estimated that the wing would 32 ° and ASTRONAUTICS aircraft , with the exception of the ...
32. oldal
Two- spar wing with third spar Over centre- section and inner wings . Naturally aged Al - Cu alloys for skins and stringers . Two- Circular - section_monocoque fuselage . spar wing in five sections including centre- section continuous ...
Two- spar wing with third spar Over centre- section and inner wings . Naturally aged Al - Cu alloys for skins and stringers . Two- Circular - section_monocoque fuselage . spar wing in five sections including centre- section continuous ...
19. oldal
0.75 EXPERIMENT : R 125 025 TRANSVERSE PROFILE AT LEADING EDGE OF SWEPT WING -TRANSVERSE PROFILE AT TRAILING EDGE OF ... flow should be feasible on swept wings laminarized by suction with somewhat increased suction quantities compared ...
0.75 EXPERIMENT : R 125 025 TRANSVERSE PROFILE AT LEADING EDGE OF SWEPT WING -TRANSVERSE PROFILE AT TRAILING EDGE OF ... flow should be feasible on swept wings laminarized by suction with somewhat increased suction quantities compared ...
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