Determination of loads in the ultralight helicopter blades
The article describes research that was carried out on coaxial a single-seat ultralight helicopter Rotorschmiede VA-115 which is manufactured by German firm RS Helikopter GmbH. The purpose of the work was to determine the blades’ loads necessary for further blade fatigue analysis and ground bench t...
Main Author: | Vitaly Dudnik |
---|---|
Format: | Article |
Language: | English |
Published: |
Vilnius Gediminas Technical University
2023-11-01
|
Series: | Aviation |
Subjects: | |
Online Access: | https://mma.vgtu.lt/index.php/Aviation/article/view/20236 |
Similar Items
-
DETERMINATION OF OPTIMAL AZIMUTH FOR MOUNTING ULTRALIGHT COAXIAL HELICOPTER BLADES
by: Vitaly V. Dudnik, et al.
Published: (2011-06-01) -
Determination of the Tail Unit Parameters of Ultralight Manned and Unmanned Helicopters at the Preliminary Design Stage
by: Vitaly Dudnik
Published: (2025-01-01) -
Reduction of torque pulsation in ultralight helicopter transmission
by: Vitaly Dudnik
Published: (2024-03-01) -
Effect of surface roughness on helicopter main rotor blade
by: W. N., W. Rohizan, et al.
Published: (2016) -
SIMULATION AND OPTIMIZATION OF ULTRALIGHT HELICOPTER AERODYNAMIC CHARACTERISTICS
by: Viktor P. Zharov, et al.
Published: (2012-08-01)