NAVAIRDEVCEN Graphite-Epoxy Composite Wing for BQM-34E:Aeroelastic Analysis.

摘要

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)