Design and principal advantages; high lift obtained without increasing total drag by using deep high-lift section for top wing and medium section for bottom wing; gives greater efficiency.
"Gloster" high lift biplane wings
Nat. Advisory Committee Aeronautics -- Tech. Memorandum
1927
5 pages
2 Figs.
Report
English
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"Gloster" high lift biplane wings
NTRS | 1927
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