The Level 16 flutter analysis capability was applied to an aspect-ratio-6.8 subsonic transport type wing, an aspect-ratio-1.7 arrow wing, and an aspect-ratio-1.3 all movable horizontal tail with a geared elevator. The transport wing and arrow wing results are compared with experimental results obtained in the Langley transonic dynamic tunnel and with other calculated results obtained using subsonic lifting surface (kernel function) unsteady aerodynamic theory.
Some applications of the NASTRAN level 16 subsonic flutter analysis capability
1976-10-01
Conference paper
No indication
English
NASTRAN cyclic symmetry capability user's guide
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New Element Definition Capability for NASTRAN
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|The numerical simulation of subsonic flutter
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|Nastran User's Guide (Level 17.5)
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