THE EFFECT OF SHEET THICKNESS ON FLIGHT SIMULATION FATIGUE CRACK PROPAGATION IN 2024-T3, 7475-T761 AND MILL ANNEALED TI-6A1-4V.
- Author
- WANHILL RJH
- Source
- J. SOC. ENVIRONMENT. ENGRS; GBR; DA. 1978; VOL. 17; NO 2; PP. 27-32; BIBL. 24 REF.
- Document type
- Article
- Language
- English
- Keyword (fr)
- FATIGUE TITANE 50-100 ALUMINIUM 50-100 PROPAGATION FISSURE EPAISSEUR ESSAI FATIGUE CHARGE PROGRAMMEE TOLE METALLURGIE
- Keyword (en)
- FATIGUE CRACK PROPAGATION THICKNESS FATIGUE TEST PROGRAMMED LOAD SHEET METAL METALLURGY
- Keyword (es)
- METALURGIA
- Classification
- Discipline
- Metals. Metallurgy
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7900027412
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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