Modelling and Attenuation Feasibility of the Aeroelastic Response of Active Helicopter Rotor Systems During the Engagement/Disengagement Phase of Maritime Operation

doi 10.22215/etd/2009-06257
Full Text
Abstract

Available in full text

Date

Unknown

Authors
Publisher

Carleton University

Related search

Modelling and Stability Analysis of a Composite Helicopter Rotor Blade With Integrated Active Fibres

English

Feasibility Study and Design of an Actively Controlled Tip for Helicopter Rotor Blades

English

Fast Modelling and Simulation of the Dynamic Behaviour of a Wet Multidisc Clutch During the Engagement Phase

MATEC Web of Conferences
Materials ScienceEngineeringChemistry
2019English

A Full-Scale Experimental Feasibility Study of Helicopter Rotor Isolation Using the Dynamic Antiresonant Vibration Isolator

1971English

Aeroelastic Response Characteristics of a Hovering Rotor Due to Harmonic Blade Pitch Variation.

Journal of the Japan Society for Aeronautical and Space Sciences
1988English

Aeroelastic and Aeroacoustic Modelling of Rotorcraft

English

Aeroelastic Rotor Stability Analysis

1976English

Aerodynamic/Acoustic Analysis for Main Rotor and Tail Rotor of Helicopter

Transactions of the Japan Society for Aeronautical and Space Sciences
SpacePlanetary ScienceAerospace Engineering
2008English

Approximations of Aeroelastic Steady State Response of Teetered Rotor Blades. (Including Teeter Rotation Argle Alone).

Nippon Kikai Gakkai Ronbunshu, C Hen/Transactions of the Japan Society of Mechanical Engineers, Part C
Mechanics of MaterialsIndustrialMechanical EngineeringManufacturing Engineering
1989English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2026 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy