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Helicopter rotor hub vibration reduction using passive methods

Turumella, Anil Yasasvi (2024) Helicopter rotor hub vibration reduction using passive methods. DLR-Interner Bericht. DLR-IB-FT-BS-2024-43. Ernst-Abbe-Fachhochschule Jena, University of Applied Sciences. 16 S.

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Abstract

In order to reduce helicopter rotor hub vibration, an optimization procedure was developed which involves integrating VAST (Versatile Aerodynamic Simulation Tool) into the workflow-integrated environment RCE (Remote Control Environment) and using a Single-Objective Genetic optimization algorithm as the optimizer

Item URL in elib:https://elib.dlr.de/207160/
Document Type:Monograph (DLR-Interner Bericht)
Title:Helicopter rotor hub vibration reduction using passive methods
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Turumella, Anil YasasviUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2024
Open Access:Yes
Number of Pages:16
Status:Published
Keywords:Vibration reduction, Helicopter rotor, tuning masses, optimization
Institution:Ernst-Abbe-Fachhochschule Jena, University of Applied Sciences
Department:Department SciTec
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Rotorcraft and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Flight Systems
Deposited By: Majeti, Rohin Kumar
Deposited On:20 Nov 2024 19:15
Last Modified:04 Mar 2025 15:44

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