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
Institution University of New Hampshire
Cites: 18
Cited by: 3
Related to: 10
FWCI:
Citation percentile (by year/subfield): 60.68
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: hybrid
APC paid (est): $2,400
Funder National Science Foundation
Grant ID DMS-0604842