The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing experiments with straight wings (zero dihedral), wings with dihedral, and wings with sweepback are evaluated within the range of sound angles of attack, explained by calculation and generally enlarged.
Forces and moments on a yawed airfoil
1939-08-01
Miscellaneous
No indication
English
Forces and moments on a yawed airfoil by Sighard Hoerner
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