Framework for Establishing Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis (2011)
Attributed to:
Supercomputing Resources and Support for the UK Applied Aerodynamics Consortium 2 (2007-2010)
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.2514/1.c001003
Publication URI: http://dx.doi.org/10.2514/1.c001003
Type: Journal Article/Review
Parent Publication: Journal of Aircraft
Issue: 1