Formulas and curves are given for elliptic, straight tapered and trapezoidal wings, based on modified form of Schrenk distribution of lift; comparison with experimental curves for derivatives shows that method gives good agreement and enables reasonably accurate estimation of rolling performance of aircraft to be made.
Rolling performance of aircraft
Aircraft Eng
Aircraft Engineering ; 20 , n 232
1948
Aufsatz (Zeitschrift)
Englisch
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Rolling Performance of Aircraft
Emerald Group Publishing | 1948
|Engineering Index Backfile | 1961
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