Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint

A Manes; Daniele Colombo; M Giglio

Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint

A Manes
, Daniele Colombo
, M Giglio

The University of Manchester

Research output: Chapter in Book/Conference proceeding › Conference contribution

Abstract

Aerospace structures need excellent structural efficiency. The advantages of Al-Li alloys over conventional aluminium alloys include relatively low densities, high elastic modulus, excellent fatigue and toughness properties, and superior fatigue crack gro

Original language	English
Title of host publication	Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint
Publication status	Published - 14 May 2006
Event	Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA - Duration: 14 May 2006 → …

Conference

Conference	Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA
Period	14/05/06 → …

Cite this

@inproceedings{66c4e5cfb9c74724b07fbc9b2e062182,

title = "Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint",

abstract = "Aerospace structures need excellent structural efficiency. The advantages of Al-Li alloys over conventional aluminium alloys include relatively low densities, high elastic modulus, excellent fatigue and toughness properties, and superior fatigue crack gro",

author = "A Manes and Daniele Colombo and M Giglio",

year = "2006",

month = may,

day = "14",

language = "English",

booktitle = "Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint",

note = "Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA ; Conference date: 14-05-2006",

}

TY - GEN

T1 - Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint

AU - Manes, A

AU - Colombo, Daniele

AU - Giglio, M

PY - 2006/5/14

Y1 - 2006/5/14

N2 - Aerospace structures need excellent structural efficiency. The advantages of Al-Li alloys over conventional aluminium alloys include relatively low densities, high elastic modulus, excellent fatigue and toughness properties, and superior fatigue crack gro

AB - Aerospace structures need excellent structural efficiency. The advantages of Al-Li alloys over conventional aluminium alloys include relatively low densities, high elastic modulus, excellent fatigue and toughness properties, and superior fatigue crack gro

M3 - Conference contribution

BT - Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint

T2 - Fatigue 2006, 9th International Fatigue Congress - Atlanta, Georgia, USA

Y2 - 14 May 2006

ER -

Experimental and numerical approach in fatigue life prediction for an Al8090 helicopter bolted joint

Abstract

Conference

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