Aeroelastic simulation of tilt-rotors using non-linear finite element multibody procedures

C. L. Bottasso

doi:10.1016/B978-008044046-0.50311-0

Aeroelastic simulation of tilt-rotors using non-linear finite element multibody procedures

C. L. Bottasso

Politecnico di Milano

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

2 Scopus citations

Abstract

The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.

Original language	English
Title of host publication	Computational Fluid and Solid Mechanics 2003
Publisher	Elsevier Inc.
Pages	1267-1270
Number of pages	4
ISBN (Electronic)	9780080529479
ISBN (Print)	9780080440460
DOIs	https://doi.org/10.1016/B978-008044046-0.50311-0
State	Published - 2 Jun 2003
Externally published	Yes

Keywords

Aeroelasticity
Finite elements
Flutter
Multibody dynamics
Rotorcraft vehicles

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10.1016/B978-008044046-0.50311-0

Cite this

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title = "Aeroelastic simulation of tilt-rotors using non-linear finite element multibody procedures",

abstract = "The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.",

keywords = "Aeroelasticity, Finite elements, Flutter, Multibody dynamics, Rotorcraft vehicles",

author = "Bottasso, {C. L.}",

year = "2003",

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AU - Bottasso, C. L.

PY - 2003/6/2

Y1 - 2003/6/2

N2 - The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.

AB - The finite element multibody technique is applied to the aeroelastic modeling of tilt-rotors. We analyze the model of a realistic aircraft configuration, and we compare alternative techniques for measuring its aeroelastic stability.

KW - Aeroelasticity

KW - Finite elements

KW - Flutter

KW - Multibody dynamics

KW - Rotorcraft vehicles

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U2 - 10.1016/B978-008044046-0.50311-0

DO - 10.1016/B978-008044046-0.50311-0

M3 - Chapter

AN - SCOPUS:84941619548

SN - 9780080440460

SP - 1267

EP - 1270

BT - Computational Fluid and Solid Mechanics 2003

PB - Elsevier Inc.

ER -

Aeroelastic simulation of tilt-rotors using non-linear finite element multibody procedures

Abstract

Keywords

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