Evaluation of Modeling Accuracy of Aircraft Wing Aerodynamic Parameters on the Basis of Measurement Results

The aim of this research is to develop and examine a method for analysis of aerodynamic parameters of the aircraft wing based on the airfoil measurement results and mathematical simulation using non-linear characteristics of airfoils constituting the wing. === Pilotuojamiems orlaiviams keliami vieno...

Full description

Bibliographic Details
Main Author: Pakalnis, Egidijus
Other Authors: Giniotis, Vytautas
Format: Doctoral Thesis
Language:English
Published: Lithuanian Academic Libraries Network (LABT) 2006
Subjects:
Online Access:http://vddb.library.lt/fedora/get/LT-eLABa-0001:E.02~2005~D_20060213_220011-43659/DS.005.1.01.ETD