Correlation of AH-1G Airframe Flight Vibration Data with a Coupled Rotor-fuselage Analysis

Correlation of AH-1G Airframe Flight Vibration Data with a Coupled Rotor-fuselage Analysis PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 232

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Correlation of AH-1G Airframe Flight Vibration Data with a Coupled Rotor-fuselage Analysis

Correlation of AH-1G Airframe Flight Vibration Data with a Coupled Rotor-fuselage Analysis PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 232

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Summary of AH-1G Flight Vibration Data for Validation of Coupled Rotor-fuselage Analyses

Summary of AH-1G Flight Vibration Data for Validation of Coupled Rotor-fuselage Analyses PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 166

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Coupled Rotor/fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight Vibrations Data

Coupled Rotor/fuselage Dynamic Analysis of the AH-1G Helicopter and Correlation with Flight Vibrations Data PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 156

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Correlation of Ah-1g Airframe Flight Vibration Data with a Coupled Rotor-Fuselage Analysis

Correlation of Ah-1g Airframe Flight Vibration Data with a Coupled Rotor-Fuselage Analysis PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781723548345
Category :
Languages : en
Pages : 228

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The formulation and features of the Rotor-Airframe Comprehensive Analysis Program (RACAP) is described. The analysis employs a frequency domain, transfer matrix approach for the blade structural model, a time domain wake or momentum theory aerodynamic model, and impedance matching for rotor-fuselage coupling. The analysis is applied to the AH-1G helicopter, and a correlation study is conducted on fuselage vibration predictions. The purpose of the study is to evaluate the state-of-the-art in helicopter fuselage vibration prediction technology. The fuselage vibration predicted using RACAP are fairly good in the vertical direction and somewhat deficient in the lateral/longitudinal directions. Some of these deficiencies are traced to the fuselage finite element model. Sangha, K. and Shamie, J. Unspecified Center NASA-CR-181974, NAS 1.26:181974 NAS1-17498; RTOP 505-63-51-01...

A Historical Overview of Aeroelasticity Branch and Transonic Dynamics Tunnel Contributions to Rotorcraft Technology and Development

A Historical Overview of Aeroelasticity Branch and Transonic Dynamics Tunnel Contributions to Rotorcraft Technology and Development PDF Author:
Publisher: DIANE Publishing
ISBN: 1428995803
Category :
Languages : en
Pages : 115

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1036

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Summary of the Modeling and Test Correlations of a NASTRAN Finite Element Vibrations Model for the AH-1G Helicopter, Task 1

Summary of the Modeling and Test Correlations of a NASTRAN Finite Element Vibrations Model for the AH-1G Helicopter, Task 1 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 304

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A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program

A Government/Industry Summary of the Design Analysis Methods for Vibrations (DAMVIBS) Program PDF Author:
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 68

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Calculation of Flight Vibration Levels of the AH-1G Helicopter and Correlation with Existing Flight Vibration Measurements

Calculation of Flight Vibration Levels of the AH-1G Helicopter and Correlation with Existing Flight Vibration Measurements PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 212

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The NASA/industry Design Analysis Methods for Vibrations (DAMVIBS) Program: A Government Overview

The NASA/industry Design Analysis Methods for Vibrations (DAMVIBS) Program: A Government Overview PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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