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Method of reducing design aerodynamic characteristics to the results of drain tests of a transport category aircraft model
- Authors: Bondar Y.I.1
-
Affiliations:
- National Technical University of Ukraine “Kiev Polytechnic Institute”
- Issue: Vol 13, No 1 (2014)
- Pages: 22-29
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1694
- DOI: https://doi.org/10.18287/1998-6629-2014-0-1(43)-22-29
- ID: 1694
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Abstract
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.
Email: bomis@meta.ua
Senior Lecturer
Department of Aerospace System
UkraineReferences
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