Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model


A method of reducing design aerodynamic characteristics to the results of drain tests by adjusting a mathematical model of the aircraft being designed on the basis of an aerodynamic prototype is presented in the paper.

About the authors

Yu. I. Bondar

National Technical University of Ukraine “Kiev Polytechnic Institute”

Author for correspondence.


Senior Lecturer

Department of Aerospace System


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