It is shown that lift distribution for biplane with unequal chords may be calculated by method developed in NACA Tech Report n 458, indexed in Engineering Index 1933 p 40, if corrections are made for inequality of chord lengths, method applied to four cases. (5¢)
Relative loading on biplane wings of unequal chords
Nat Advisory Committee Aeronautics -- Report
1934
8 pages
Bibliography
Report
Englisch
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Relative loading on biplane wings of unequal chords
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