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PRACTICAL METHOD OF FATIGUE CRACK GROWTH ANALYSIS FOR DAMAGE TOLERANCE ASSESSMENT OF ALUMINUM STRUCTURE IN FIGHTER-TYPE AIRCRAFT

Other title
METHODE PRATIQUE POUR L'ANALYSE DES FISSURES DE FATIGUE POUR L'EVALUATION DES DOMMAGES TOLERABLES DES STRUCTURES D'AL UTILISEES DANS LES AVIONS (fr)
Author
LEVY M; KUO AS; GRUBE K
FAIRCHILD REPUBLIC CO./FARMINGDALE NY/USA
Source
AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 9 P.; BIBL. 22 REF.
Document type
Conference Paper
Language
English
Keyword (fr)
FATIGUE PROPAGATION FISSURE MODELE MATHEMATIQUE INDUSTRIE AERONAUTIQUE ALLIAGEM AL:>50 METALLURGIE
Keyword (en)
FATIGUE CRACK PROPAGATION MATHEMATICAL MODELS AERONAUTIC INDUSTRY METALLURGY
Keyword (es)
METALURGIA
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D11 Metals. Metallurgy

Discipline
Metals. Metallurgy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL8100231457

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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