A final aeroelastic analysis of the NAVAIRDEVCEN advanced graphite-epoxy composite wing for the unmanned supersonic BQM-34E aerial target indicates flutter free behavior within the 15% margin flight envelope. The wing is also divergent free throughout the flight regime and exhibits an expected forward and inboard shift of the aerodynamic center of pressure. (Author)
NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E: Aeroelastic Analysis
1973
19 pages
Report
Keine Angabe
Englisch
Static aeroelastic analysis of composite wing
NTRS | 1990
|Uncertainty of Composite Wing Aeroelastic Behaviour
British Library Conference Proceedings | 2008
|Swept composite wing aeroelastic divergence experiments
AIAA | 1982
|Aeroelastic Analysis of Composite Wing with Control Surface
British Library Online Contents | 1992
|