The vortex flow over an arrow wing is theoretically investigated using the free-vortex-sheet method. The sectional lift coefficient and accumulated span loadings, which are important in determining the root bending moment, are calculated. The longitudinal stability variation is also estimated.
Accumulated span loadings of an arrow wing having vortex flow
Journal of Aircraft ; 26
01.11.1989
Sonstige
Keine Angabe
Englisch
Vortex Structures and Span Loadings from Alleviated-Wake Measurement3
British Library Conference Proceedings | 1997
|Emerald Group Publishing | 1977
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