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
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