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Journal Nonlinear World №1 for 2017 г.
Article in number:
Theoretical basis for design, development and experimental studies of the helicopter air data system on the basis of the fixed multifunctional aerometric receiver
Keywords: helicopter air data system vortex column aerodynamic field aerodynamic receiver fixed spatially-distributed theoretical basis for design development experimental studies wind tunnel
Authors:
V.V. Soldatkin - Dr.Sc. (Eng.), Associate Professor, Department of Devices and Information-Measuring Systems, Kazan National Research Technical University named after A.N. Tupolev E-mail: w-soldatkin@mail.ru
Abstract:
The approaches to use, formation and perception of information aerodynamic field of vortex column of main rotor with a fixed spatially-distributed aerometric receiver and processing it in the channels of the system air data signals helicopter are considered. The results of development and experimental studies of the system in the wind tunnel are produced.
Pages: 58-65
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