Some of the single rotation propfan model wind tunnel aeroelastic findings from the experimental part of this research program are described. These findings include results for unstalled or classical flutter, blade response from separated flow excitations, and blade response from aerodynamic excitations at angled inflow conditions.
Propfan Model Wind Tunnel Aeroelastic Research Results
1988
14 pages
Report
Keine Angabe
Englisch
Composite-Material Propfan Blades for a Wind-Tunnel Model
Online Contents | 1995
Aeroacoustic Wind Tunnel Testing of a Counterrotating Shrouded Propfan Model
British Library Conference Proceedings | 1992
|Structural and aeroelastic analysis of the SR-7L propfan
NTRS | 1985
|Aeroelastic effects of alternate blade sweep on advanced propfan rotor
Tema Archiv | 1987
|