DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING
Abstract
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 derivative factors of elevating force and aerodynamic resistance of a wing under the appropriate characteristics of a profile.
References
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Review
For citations:
Artamonov B.L. DEFINITION OF AERODYNAMIC CHARACTERISTICS OF THE PROFILE UNDER THE DRAG POLAR OF THE FINITE WING. Civil Aviation High Technologies. 2014;(200):28-35. (In Russ.)
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