Some early experimental results from a combined experimental and analytical study being conducted at NASA-Langley of the transonic flutter characterisitics of a generic arrow wing configuration are presented. The planned study includes the parametric variation of a variety of structural and geometric characteristics. Presented here are flutter results of the basic arrow wing, for the basic wing with the addition of two simulated lower-surface-mounted engine nacelles, and for the basic wing with the addition of both the fin and the engine nacelles.
Parametric flutter studies of an arrow-wing configuration: Some early results
1988-05-01
Report
No indication
English
Scar Arrow-Wing Active Flutter Suppression System
NTIS | 1977
|SCAR arrow-wing active flutter suppression system
NTRS | 1977
|