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Numerical Investigation of Aeroelastic Mode Distribution for Aircraft Wing Model in Subsonic Air Flow
Work
Year: 2010
Type: article
Abstract: In this paper, the numerical results on two problems originated in aircraft wing modeling have been presented. The first problem is concerned with the approximation to the set of the aeroelastic modes... more
Cites: 18
Cited by: 3
Related to: 10
FWCI:
Citation percentile (by year/subfield): 60.68
Open Access status: hybrid
APC paid (est): $2,400
Grant ID DMS-0604842