Aeroelastic Analysis of the Elastic Gimbal Rotor PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
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Book Description
The Elastic Gimbal Rotor (EGR) is a new Sikorsky concept in helicopter rotor systems. The EGR uses essentially bearingless rotor blades attached to a rotor head which is able to tilt relative to the rotor shaft. The tilt motion about the gimbal bearing is restrained by an elastically deformable member of members which form part of the hub. This spring restraint action permits hub moments to be transferred from the rotor blades to the main rotor shaft. This program was a preliminary study of the elastic gimbal rotor. The emphais was on the dynamic loads and the aeroelastic response of the system.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116
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Book Description
The Elastic Gimbal Rotor (EGR) is a new Sikorsky concept in helicopter rotor systems. The EGR uses essentially bearingless rotor blades attached to a rotor head which is able to tilt relative to the rotor shaft. The tilt motion about the gimbal bearing is restrained by an elastically deformable member of members which form part of the hub. This spring restraint action permits hub moments to be transferred from the rotor blades to the main rotor shaft. This program was a preliminary study of the elastic gimbal rotor. The emphais was on the dynamic loads and the aeroelastic response of the system.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 910
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Book Description
Author: Wayne Johnson
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 260
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 188
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 808
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Book Description
Author:
Publisher:
ISBN:
Category : Aeroelasticity
Languages : en
Pages : 460
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Book Description
These proceedings represent a collection of the latest advances in aeroelasticity and structural dynamics from the world community. Research in the areas of unsteady aerodynamics and aeroelasticity, structural modeling and optimazation, active control and adaptive structures, landing dynamics, certification and qualification, and validation testing are highlighted in the collection of papers. The wide range of results will lead to advances in the prediction and control of the structural response of aircraft and spacecraft.
Author:
Publisher: DIANE Publishing
ISBN: 1428995803
Category :
Languages : en
Pages : 115
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Book Description
Author: United States. President
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 100
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Author: United States. President
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 430
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 554
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Book Description
