Effects of Compressibility on Maximum Lift Characteristics and Spanwise Load Distribution on 12-FootSpan Fighter-Type Wing of NACA 230-Series Airfoil Sections. (Originally issued as Advance Confidential Report L5G10)
Effects of compressibility on maximum lift characteristics and spanwise load distribution on 12-footspan fighter-type wing of NACA 230-series airfoil sections
Nat Advisory Committee Aeronautics -- Wartime Report
1945
13 pages
14 Supp plates
Report
English
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Engineering Index Backfile | 1948
|Engineering Index Backfile | 1947
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