Analysis of Residual Stress Effect on Fatigue Crack Propagation in Bonded Aeronautical Stiffened Panels: Fid-Bau Portal

Analysis of Residual Stress Effect on Fatigue Crack Propagation in Bonded Aeronautical Stiffened Panels

Meneghin, I. / Ivetic, G. / Troiani, E.

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Analysis of Residual Stress Effect on Fatigue Crack Propagation in Bonded Aeronautical Stiffened Panels

Meneghin, I. / Ivetic, G. / Troiani, E.

Analysis of Residual Stress Effect on Fatigue Crack Propagation in Bonded Aeronautical Stiffened Panels

Meneghin, I. / Ivetic, G. / Troiani, E.

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Check availability in my library

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Document information

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Document information

Title:

Analysis of Residual Stress Effect on Fatigue Crack Propagation in Bonded Aeronautical Stiffened Panels

Contributors:

Meneghin, I. (author) / Ivetic, G. (author) / Troiani, E. (author) / Scardi, P. / Ricardo, C.L.A.

Published in:

Residual Stresses VIII ; 236-242

MATERIALS SCIENCE FORUM ; 681

Publication date:

2011-01-01

Size:

7 pages

ISSN:

0255-5476

Type of media:

Article (Journal)

Type of material:

Language:

English

Classification:

DDC: 620.11

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