It is shown that the lift distribution for a biplane with unequal chords may be calculated by the method developed in NACA Technical report no. 458 if corrections are made for the inequality in chord lengths. The method is applied to four cases in which the upper chord was greater than the lower and good agreement is obtained between observed and calculated lift coefficients.
Relative loading on biplane wings of unequal chords
01.01.1935
Sonstige
Keine Angabe
Englisch
Relative loading on biplane wings of unequal chords
Engineering Index Backfile | 1934
|Relative loading on biplane wings of unequal chords
TIBKAT | 1934
|Relative loading on biplane wings
TIBKAT | 1933
|Relative loading on biplane wings
Engineering Index Backfile | 1933
|Convertible monoplane -- Biplane wings
Engineering Index Backfile | 1926
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