Experimental investigation of main rotor wake
In this work, experimental results of rotor wake in hover mode are presented. The experiments were carried out with a rotor rig model in the T-1K wind tunnel in Kazan National Research Technical University (Kazan Aviation Institute). The rotor consisted of four identical blades. The Q-criterion was...
Main Authors: | Stepanov Robert, Mikhailov Sergey |
---|---|
Format: | Article |
Language: | English |
Published: |
EDP Sciences
2017-01-01
|
Series: | MATEC Web of Conferences |
Online Access: | https://doi.org/10.1051/matecconf/201711502013 |
Similar Items
-
Main Rotor Wake Interference Effects on Tail Rotor Thrust in Crosswind
by: Chang Wang, et al.
Published: (2021-01-01) -
Unsteady aerodynamic wake of helicopter main-rotor-hub assembly
by: Ishak, Iskandar Shah
Published: (2012) -
Numerical studies on unsteady helicopter main-rotor-hub assembly wake
by: Ishak, Iskandar Shah, et al.
Published: (2018) -
CAA modeling of helicopter main rotor in hover
by: Kusyumov Alexander N., et al.
Published: (2017-01-01) -
COMPUTATIONAL STUDY OF AERODYNAMIC CHARACTERISTICS OF SINGLE-ROTOR HELICOPTER TAIL ROTOR UNDER THE INFLUENCE OF VORTICAL WAKE OF MAIN ROTOR AT THE HOVER WITH CROSSWIND
by: Yu. M. Ignatkin, et al.
Published: (2017-01-01)