ALGORITHM OF MESH DEFORMATION FOR ACCOUNTING CYCLIC BLADE CONTROL AND BLADES FLAPPING IN THE PROBLEM OF HELICOPTER MAIN ROTOR MODELING

ALGORITHM OF MESH DEFORMATION FOR ACCOUNTING CYCLIC BLADE CONTROL AND BLADES FLAPPING IN THE PROBLEM OF HELICOPTER MAIN ROTOR MODELING

This paper presents the developed algorithm for numerical grid deformation for solving the problems of modeling the flow around the helicopter main rotor in the horizontal flight mode with allowance for flapping movements and cyclic changes in the angle of the blade installation. In general, this al...

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Bibliographic Details
Main Author: V. A. Vershkov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2019-04-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
helicopter main rotor
grid deformation
blade balancing
blade flapping
blade pitching
Online Access:https://avia.mstuca.ru/jour/article/view/1480

Internet

https://avia.mstuca.ru/jour/article/view/1480

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