Unwanted Supplementary Vibrations of Helicopter Radio Communication Systems
Author:
Affiliation:
1. Faculty of Aeronautics, Technical University of Košice, Rampová 7, 041 21 Košice, Slovakia
2. Faculty of Mechanical Engineering, Technical University of Košice, Letná 1/9, 042 00 Košice, Slovakia
Abstract
Funder
KEGA
Publisher
MDPI AG
Subject
Aerospace Engineering
Link
https://www.mdpi.com/2226-4310/10/7/632/pdf
Reference41 articles.
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2. Tommasino, D., Moro, F., Zumalde, E., Kunzmann, J., and Doria, A. (2023). An Analytical–Numerical Method for Simulating the Performance of Piezoelectric Harvesters Mounted on Wing Slats. Actuators, 12.
3. Study on the lift and propulsive force shares to improve the flight performance of a compound helicopter;Yang;Chin. J. Aeronaut.,2021
4. Cumbo, R., Tamarozzi, T., Jiranek, P., Desmet, W., and Masarati, P. (2020). State and Force Estimation on a Rotating Helicopter Blade through a Kalman-Based Approach. Sensors, 20.
5. Aerodynamics and flight mechanics analysis of Airbus Helicopters’ compound helicopter RACER in hover under crosswind conditions;Thiemeier;CEAS Aeronaut. J.,2019
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