Research on aeroelastic tailoring at NAL is presented. Flutter boundaries for an optimized forward swept wing have been experimentally verified at angles of attack of 0 and 2 degrees (which is the design point) in the transonic range. It was found that two different mode flutters and a divergence occur at almost the same dynamic pressure for the optimized forward swept wing. The aeroelastic behavior of the optimized forward swept wing is investigated and is compared with that of parametric studies performed previously.
Aeroelastic Characteristics of the Forward Swept Wing Optimized by Aeroelastic Tailoring
1993
15 pages
Report
Keine Angabe
Englisch
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