DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING
The numerical method of calculation of aerodynamic characteristics of a profile is stated on the basis of the experiment of aerodynamic characteristics of a rectangular wing of a final lengthening. The problem is solved by a method consecutive approximation with the use of a matrix of private deriva...
Main Author: | B. L. Artamonov |
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Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
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Series: | Naučnyj Vestnik MGTU GA |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/6 |
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