Induced-Drag Calculations in the Unsteady Vortex Lattice Method (2013)
Attributed to:
Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/1.j052136
Publication URI: http://dx.doi.org/10.2514/1.j052136
Type: Journal Article/Review
Parent Publication: AIAA Journal
Issue: 7