EXPERIMENTAL RESEARCH OF INFLUENCE OF SITES SIZE RESTRICTIONS ON AERODYNAMIC CHARACTERISTICS OF THE ROTOR
The analysis of the impact of limited size areas on the aerodynamic characteristics of the rotor obtained using previous studies and some of the results of modern experimental research are given.
Main Authors: | E. A. Borisov, V. A. Leontiev, N. N. Tarasov |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/132 |
Similar Items
-
Thrust pulsation of coaxial main rotor, caused by the blades relative position
by: B. S. Kritsky, et al.
Published: (2020-09-01) -
THE EFFECT OF DIFFERENT OPTIONS OF BLADES MAIN ROTOR ON THE X-SHAPED TAIL ROTOR OF THE MI-171 LL
by: V. A. Ivchin, et al.
Published: (2018-03-01) -
CALCULATION OF LOADS ON THE CONTROLS WITH HELICOPTER MAIN ROTOR OF SINGLE-ROTOR DESIGN
by: B. L. Artamonov, et al.
Published: (2016-11-01) -
COMPUTATIONAL MODELING OF AERODYNAMIC INTERFERENCE OF HELICOPTER MAIN AND TAIL ROTORS AT THE SPECIAL FLIGHT REGIMES
by: Y. M. Ignatkin, et al.
Published: (2016-11-01) -
PRESSURE THEORY OF HELICOPTER ROTOR
by: Sergey P. Lisin
Published: (2011-09-01)