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- W3030941210 abstract "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." @default.
- W3030941210 created "2020-06-05" @default.
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- W3030941210 date "1976-10-01" @default.
- W3030941210 modified "2023-09-23" @default.
- W3030941210 title "Some applications of the NASTRAN level 16 subsonic flutter analysis capability" @default.
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