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INTRODUCTION OF CERAMICS INTO AEROSPACE STRUCTURAL COMPOSITE.(L'Introduction des Céramiques dans les Composites Utilisés dans les Structures des Systèmes Aérospatiaux).
Titre : INTRODUCTION OF CERAMICS INTO AEROSPACE STRUCTURAL COMPOSITE.(L'Introduction des Céramiques dans les Composites Utilisés dans les Structures des Systèmes Aérospatiaux). Type de document : document imprimé Editeur : ONERA Année de publication : 34274 Collection : (AGARD-R-795). Importance : 160,00 ISBN/ISSN/EAN : 92-8350-728-2 Langues : Français (fre) Mots-clés : AEROSPACE ENGINEERING AIRCRAFT ENGINES CERAMIC COMPOSITES CRACK PROPAGATION FATIGUE MATERIALS FIBER LAMINATES FRACTURE MECHANICS GLASS MATRIX COMPOSITE MISSILES STRUCTURAL COMPONENTS Note de contenu : Workshop held by the AGARD Structures and Materials Panel,in Antalya,Turkey, 21th-22nd April 93
INTRODUCTION OF CERAMICS INTO AEROSPACE STRUCTURAL COMPOSITE.(L'Introduction des Céramiques dans les Composites Utilisés dans les Structures des Systèmes Aérospatiaux). [document imprimé] . - ONERA, 34274 . - 160,00. - ((AGARD-R-795).) .
ISBN : 92-8350-728-2
Langues : Français (fre)
Mots-clés : AEROSPACE ENGINEERING AIRCRAFT ENGINES CERAMIC COMPOSITES CRACK PROPAGATION FATIGUE MATERIALS FIBER LAMINATES FRACTURE MECHANICS GLASS MATRIX COMPOSITE MISSILES STRUCTURAL COMPONENTS Note de contenu : Workshop held by the AGARD Structures and Materials Panel,in Antalya,Turkey, 21th-22nd April 93
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Code-barres Cote Support Localisation Section Disponibilité MA2274 Document imprimé Bureau chercheur Indéterminé Disponible FIBER OPTICS. / KAPANY N.S.
Titre : FIBER OPTICS. Type de document : document imprimé Auteurs : KAPANY N.S., Auteur Editeur : Academic Press Année de publication : 1967 Importance : 429,00 Langues : Français (fre) Mots-clés : FIBER LASER FIBER OPTICS APPLICATIONS FIBER OPTICS TECHNOLOGY GEOMETRICAL OPTICS OF FIBERS OPTICAL PROPERTIES RADIATION TRANSMISSION IMAGE WAVE PROPAGATION FIBER OPTICS. [document imprimé] / KAPANY N.S., Auteur . - [S.l.] : Academic Press, 1967 . - 429,00.
Langues : Français (fre)
Mots-clés : FIBER LASER FIBER OPTICS APPLICATIONS FIBER OPTICS TECHNOLOGY GEOMETRICAL OPTICS OF FIBERS OPTICAL PROPERTIES RADIATION TRANSMISSION IMAGE WAVE PROPAGATION Réservation
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Code-barres Cote Support Localisation Section Disponibilité MA1180 Document imprimé Bureau chercheur Indéterminé Disponible RECENT DEVELOPMENTS IN NON-NEWTONIAN FLOWS AND INDUSTRIAL APPLICATIONS -1991. / DHAUBHADEL M.N SIGINER D.A
Titre : RECENT DEVELOPMENTS IN NON-NEWTONIAN FLOWS AND INDUSTRIAL APPLICATIONS -1991. Type de document : document imprimé Auteurs : DHAUBHADEL M.N SIGINER D.A, Auteur Editeur : American society of mechanical engineers, ASME Année de publication : 33573 Importance : 81,00 Langues : Français (fre) Mots-clés : FIBER-SPINNING HYDRODYNAMICS LAMINAR FLOWS NON-NEWTONIAN FLOWS NUMERICAL SIMULATION PRESSURE AND TEMPERATURE VISCOELASTIC FLUID Index. décimale : 47.85 Applied fluid mechanics, Hydrodynamics, hydraulics, hydrostatics, Aerodynamics Note de contenu : The Winter Annual Meeting of The American Society of Mechanical Engineers
RECENT DEVELOPMENTS IN NON-NEWTONIAN FLOWS AND INDUSTRIAL APPLICATIONS -1991. [document imprimé] / DHAUBHADEL M.N SIGINER D.A, Auteur . - [S.l.] : American society of mechanical engineers, ASME, 33573 . - 81,00.
Langues : Français (fre)
Mots-clés : FIBER-SPINNING HYDRODYNAMICS LAMINAR FLOWS NON-NEWTONIAN FLOWS NUMERICAL SIMULATION PRESSURE AND TEMPERATURE VISCOELASTIC FLUID Index. décimale : 47.85 Applied fluid mechanics, Hydrodynamics, hydraulics, hydrostatics, Aerodynamics Note de contenu : The Winter Annual Meeting of The American Society of Mechanical Engineers
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Code-barres Cote Support Localisation Section Disponibilité OF0063 47.85 SIG Document imprimé IRPHE Indéterminé Disponible RHEOLOGY, vol. 2. / EIRICH F.R.
Titre : RHEOLOGY, vol. 2. Type de document : document imprimé Auteurs : EIRICH F.R., Auteur Editeur : Academic Press Année de publication : 1958 Importance : 591,00 Langues : Français (fre) Mots-clés : GONIOMETRY OF FLOW RELAXATION THEORY RHEOLOGICAL PROBLEMS RHEOLOGY OF CELLULOSE RHEOLOGY OF FIBERS RHEOLOGY OF GELATIN RHEOLOGY OF ORGANIC GLASSES VISCOELASTIC BODIES VISCOELASTICITY Note de contenu : emprunte par Mr KNAPP le 05/04/95
RHEOLOGY, vol. 2. [document imprimé] / EIRICH F.R., Auteur . - [S.l.] : Academic Press, 1958 . - 591,00.
Langues : Français (fre)
Mots-clés : GONIOMETRY OF FLOW RELAXATION THEORY RHEOLOGICAL PROBLEMS RHEOLOGY OF CELLULOSE RHEOLOGY OF FIBERS RHEOLOGY OF GELATIN RHEOLOGY OF ORGANIC GLASSES VISCOELASTIC BODIES VISCOELASTICITY Note de contenu : emprunte par Mr KNAPP le 05/04/95
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Code-barres Cote Support Localisation Section Disponibilité MA1188 Document imprimé Bureau chercheur Indéterminé Disponible Textile research journal, Vol. 43, No. 12. Photographic investigation of high-speed missile impact upon nylon fabric. 1, Energy Absorption and Cone Radial Velocity in Fabric / Anthony F. Wilde
in Textile research journal / TRI/Princeton
Titre de série : Textile research journal, Vol. 43, No. 12 Titre : Photographic investigation of high-speed missile impact upon nylon fabric. 1, Energy Absorption and Cone Radial Velocity in Fabric Type de document : articles et extraits Auteurs : Anthony F. Wilde, Auteur ; David K. Roylance, Auteur ; Jos Ph M. Rogers Année de publication : 1973 Importance : p. 753-761 Langues : Anglais (eng) Mots-clés : Nylon fabric Missile impact broken orthogonal yarns High-speed photography Transient response interaction time fabric deformation cone cone radial velocity transverse wave velocity Missile energy loss energy partition fabric strain energy yarn breaking energy fabric kinetic energy energy transfer termination Fiber impact theory Résumé : Single layers of nylon fabric have been subjected to high-speed missile impact at velocities ranging from 116 to 537 m/sec. The transient responses of the fabric and missile have been observed by high-speed photography. The photo graphs have shown that fabric deformation was pyramidal before penetration and more conical after penetration. The photographs have permitted measurements of the missile exit velocity from the fabric, the missile energy loss due to interaction with the fabric, the time required to penetrate the fabric, and the size and growth rate of the resultant fabric deformation cones. These results, together with a simplified mechanical model, have indicated that the broken orthogonal yarns within the deformation cone could account for 50 100% of the observed missile energy loss. In addition, during penetration of the fabric, the measured average cone-radial velocities in the fabric ranged from 50 to 80% of the values derived from fiber impact theory.
in Textile research journal / TRI/Princeton
Textile research journal, Vol. 43, No. 12. Photographic investigation of high-speed missile impact upon nylon fabric. 1, Energy Absorption and Cone Radial Velocity in Fabric [articles et extraits] / Anthony F. Wilde, Auteur ; David K. Roylance, Auteur ; Jos Ph M. Rogers . - 1973 . - p. 753-761.
Langues : Anglais (eng)
Mots-clés : Nylon fabric Missile impact broken orthogonal yarns High-speed photography Transient response interaction time fabric deformation cone cone radial velocity transverse wave velocity Missile energy loss energy partition fabric strain energy yarn breaking energy fabric kinetic energy energy transfer termination Fiber impact theory Résumé : Single layers of nylon fabric have been subjected to high-speed missile impact at velocities ranging from 116 to 537 m/sec. The transient responses of the fabric and missile have been observed by high-speed photography. The photo graphs have shown that fabric deformation was pyramidal before penetration and more conical after penetration. The photographs have permitted measurements of the missile exit velocity from the fabric, the missile energy loss due to interaction with the fabric, the time required to penetrate the fabric, and the size and growth rate of the resultant fabric deformation cones. These results, together with a simplified mechanical model, have indicated that the broken orthogonal yarns within the deformation cone could account for 50 100% of the observed missile energy loss. In addition, during penetration of the fabric, the measured average cone-radial velocities in the fabric ranged from 50 to 80% of the values derived from fiber impact theory. Réservation
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Code-barres Cote Support Localisation Section Disponibilité ART-1973753 WIL Document imprimé Bureau chercheur Bureau de VANDENBERGHE Nicolas Disponible