COMPUTING EXPERIMENT FOR ASSESSMENT OF AERODYNAMIC CHARACTERISTICS OF SEPARATE ELEMENTS IN THE STRUCTURE OF THE FUSELAGE OF A HELICOPTER
Abstract
The present publication describes the calculation of helicopter fuselage aerodynamic characteristics and its separate elements, by computing experiment. On the basis of program commercial package CFX ANSYS the technique has been mastered and longitudinal and lateral characteristics of the helicopter fuselage on the various flight modes are calculated.
About the Authors
V. A. Ivchin
ОАО "МВЗ им. М.Л. Миля"
Russian Federation
Russian Federation
V. G. Sudakov
ОАО "МВЗ им. М.Л. Миля"
Russian Federation
Russian Federation
A. A. Ryzhov
МФТИ
Russian Federation
Russian Federation
Review
For citations:
Ivchin V.A., Sudakov V.G., Ryzhov A.A. COMPUTING EXPERIMENT FOR ASSESSMENT OF AERODYNAMIC CHARACTERISTICS OF SEPARATE ELEMENTS IN THE STRUCTURE OF THE FUSELAGE OF A HELICOPTER. Civil Aviation High Technologies. 2015;(212):82-89. (In Russ.)
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