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
- 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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