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PERFORMANCE OF ROCKET MOTORS WITH METALLIZED PROPELLANTS. / REYDELLET D.
Titre : PERFORMANCE OF ROCKET MOTORS WITH METALLIZED PROPELLANTS. Type de document : document imprimé Auteurs : REYDELLET D., Auteur Editeur : ONERA Année de publication : 32387 Collection : (AGARD-AR-230). Importance : 90,00 ISBN/ISSN/EAN : 92-8351-534-X Langues : Français (fre) Mots-clés : DIVERGENCE LOSS IMPINGEMENT LOSS METALLIZED PROPELLANT PERFORMANCE PREDICTION ROCKET MOTORS SCALE EFFECT SOLID PROPELLANT TWO PHASE FLOW Note de contenu : AGARD 7 Rue Ancelle, 92200
PERFORMANCE OF ROCKET MOTORS WITH METALLIZED PROPELLANTS. [document imprimé] / REYDELLET D., Auteur . - ONERA, 32387 . - 90,00. - ((AGARD-AR-230).) .
ISBN : 92-8351-534-X
Langues : Français (fre)
Mots-clés : DIVERGENCE LOSS IMPINGEMENT LOSS METALLIZED PROPELLANT PERFORMANCE PREDICTION ROCKET MOTORS SCALE EFFECT SOLID PROPELLANT TWO PHASE FLOW Note de contenu : AGARD 7 Rue Ancelle, 92200
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Code-barres Cote Support Localisation Section Disponibilité MA2418 Document imprimé Bureau chercheur Indéterminé Disponible HEAT TRANSFER AND COOLING IN GAS TURBINES. (Le Transfert Thermique et le refroidissement dans les Turbines à Gas).
Titre : HEAT TRANSFER AND COOLING IN GAS TURBINES. (Le Transfert Thermique et le refroidissement dans les Turbines à Gas). Type de document : document imprimé Editeur : ONERA Année de publication : 34001 Collection : (AGARD-CP-527). Importance : 510,00 ISBN/ISSN/EAN : 92-8350-701-0 Langues : Français (fre) Mots-clés : COMBUSTORS CONVECTIVE HEAT TRANSFER COOLING GAS TURBINES HEAT TRANSFER IMPINGEMENT COOLING ROTATING DISCS TURBULENT FLOW Note de contenu : Propulsion and Energetics Panel 80th Symposium held in Antalya, Turkey, 12th-16th October 93
HEAT TRANSFER AND COOLING IN GAS TURBINES. (Le Transfert Thermique et le refroidissement dans les Turbines à Gas). [document imprimé] . - ONERA, 34001 . - 510,00. - ((AGARD-CP-527).) .
ISBN : 92-8350-701-0
Langues : Français (fre)
Mots-clés : COMBUSTORS CONVECTIVE HEAT TRANSFER COOLING GAS TURBINES HEAT TRANSFER IMPINGEMENT COOLING ROTATING DISCS TURBULENT FLOW Note de contenu : Propulsion and Energetics Panel 80th Symposium held in Antalya, Turkey, 12th-16th October 93
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Code-barres Cote Support Localisation Section Disponibilité MA2267 Document imprimé Bureau chercheur Indéterminé Disponible LOSS MECHANISMS AND UNSTEADY FLOWS IN TURBOMACHINES.(les Mécanismes des pertes et les écoulements instationnaires dans les turbomachines).
Titre : LOSS MECHANISMS AND UNSTEADY FLOWS IN TURBOMACHINES.(les Mécanismes des pertes et les écoulements instationnaires dans les turbomachines). Type de document : document imprimé Editeur : ONERA Année de publication : 35065 Collection : (AGARD-CP-571). Importance : 598,00 ISBN/ISSN/EAN : 92-8360-020-7 Langues : Français (fre) Mots-clés : AIRCRAFT ENGINES BOUNDARY LAYER FLOW COMPUTATIONAL FLUID DYNAMICS LOSS MECHANISMS STEADY UNSTEADY FLOW TURBINE BLADES TURBOMACHINERY Note de contenu : Propulsion and Energetics Panel PEP 85th Symposium held in Derby, United Kingdom, 8-12 May 95
LOSS MECHANISMS AND UNSTEADY FLOWS IN TURBOMACHINES.(les Mécanismes des pertes et les écoulements instationnaires dans les turbomachines). [document imprimé] . - ONERA, 35065 . - 598,00. - ((AGARD-CP-571).) .
ISBN : 92-8360-020-7
Langues : Français (fre)
Mots-clés : AIRCRAFT ENGINES BOUNDARY LAYER FLOW COMPUTATIONAL FLUID DYNAMICS LOSS MECHANISMS STEADY UNSTEADY FLOW TURBINE BLADES TURBOMACHINERY Note de contenu : Propulsion and Energetics Panel PEP 85th Symposium held in Derby, United Kingdom, 8-12 May 95
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Code-barres Cote Support Localisation Section Disponibilité MA2305 Document imprimé Bureau chercheur Indéterminé Disponible Theory of detonation / Yakov Borisovich Zeldovich
Titre : Theory of detonation Type de document : document imprimé Auteurs : Yakov Borisovich Zeldovich, Auteur ; A. S. Kompaneets, Auteur Editeur : New York : Academic Press Année de publication : 1960 Importance : 284 p. Présentation : illus. Format : 24 cm Langues : Anglais (eng) Langues originales : Russe (rus) Mots-clés : DETONATION WAVES GAS DYNAMICS LOSSLESS COMBUSTION MOTION OF THE DETONATION SHOCK WAVES explosions Theory of detonation [document imprimé] / Yakov Borisovich Zeldovich, Auteur ; A. S. Kompaneets, Auteur . - New York : Academic Press, 1960 . - 284 p. : illus. ; 24 cm.
Langues : Anglais (eng) Langues originales : Russe (rus)
Mots-clés : DETONATION WAVES GAS DYNAMICS LOSSLESS COMBUSTION MOTION OF THE DETONATION SHOCK WAVES explosions Réservation
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Code-barres Cote Support Localisation Section Disponibilité MA1494 ZEL 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