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...
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Format: | Doctoral Thesis |
Language: | English |
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Lithuanian Academic Libraries Network (LABT)
2006
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Online Access: | http://vddb.library.lt/fedora/get/LT-eLABa-0001:E.02~2005~D_20060213_220011-43659/DS.005.1.01.ETD |