The Experts below are selected from a list of 249 Experts worldwide ranked by ideXlab platform
James E. Cocchiaro - One of the best experts on this subject based on the ideXlab platform.
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JANNAF 19th Propulsion Systems Hazards Subcommittee Meeting
2019Co-Authors: Melanie C. Kuckels, James E. CocchiaroAbstract:This volume, the first of two volumes is a compilation of 25 unclassified/unlimited-distribution technical papers presented at the Joint Army-Navy-NASA-Air Force (JANNAF) 19th Propulsion Systems Hazards Subcommittee (PSHS) meeting held jointly with the 37th Combustion Subcommittee (CS) and 25th Airbreathing Propulsion Subcommittee (APS), and 1st Modeling and Simulation Subcommittee (MSS) meetings. The meeting was held 13-17 November 2000 at the Naval Postgraduate School and Hyatt Regency Hotel, Monterey, California. Topics covered at the PSHS meeting include: impact and thermal vulnerability of gun propellants; thermal decomposition and cookoff behavior of energetic materials; violent reaction and Detonation Phenomena of solid energetic materials subjected to shock and impact loading; and hazard classification, and insensitive munitions testing of propellants and propulsion systems.
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JANNAF 19th Propulsion Systems Hazards Subcommittee Meeting. Volume 1
2000Co-Authors: James E. Cocchiaro, Melanie C. KuckelsAbstract:Abstract : This volume, the first of two volumes is a compilation of 25 unclassified/unlimited-distribution technical papers presented at the Joint Army-Navy-NASA-Air Force (JANNAF) 19th Propulsion Systems Hazards Subcommittee (PSHS) meeting held jointly with the 37th Combustion Subcommittee (CS) and 25th Airbreathing Propulsion Subcommittee (APS), and 1st Modeling and Simulation Subcommittee (MSS) meetings. The meeting was held 13-17 November 2000 at the Naval Postgraduate School and Hyatt Regency Hotel, Monterey, California. Topics covered at the PSHS meeting include: impact and thermal vulnerability of gun propellants; thermal decomposition and cookoff behavior of energetic materials; violent reaction and Detonation Phenomena of solid energetic materials subjected to shock and impact loading; and hazard classification, and insensitive munitions testing of propellants and propulsion systems.
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JANNAF 17th Propulsion Systems Hazards Subcommittee Meeting. Volume 1; Held at Raytheon Systems Company and Marriott University Park, Tucson, AZ on 7-11 December 1998
1998Co-Authors: James E. Cocchiaro, Mary T. Gannaway, Melanie RognanAbstract:Abstract : Volume I, the first of two volumes is a compilation of 16 unclassified/unlimited technical papers presented at the 17th meeting of the Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Systems Hazards Subcommittee (PSHS) held jointly with the 35th Combustion Subcommittee (CS) and Airbreathing Propulsion Subcommittee (APS). The meeting was held on 7-11 December 1998 at Raytheon Systems Company and the Marriott Hotel, Tucson, AZ. Topics covered include projectile and shaped charge jet impact vulnerability of munitions; thermal decomposition and cookoff behavior of energetic materials; damage and hot spot initiation mechanisms with energetic materials; Detonation Phenomena of solid energetic materials; and hazard classification, insensitive munitions, and propulsion systems safety.
T D Cooper - One of the best experts on this subject based on the ideXlab platform.
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spent nuclear fuel project Detonation Phenomena of hydrogen oxygen in spent fuel containers
Other Information: PBD: 30 Sep 1996, 1996Co-Authors: T D CooperAbstract:Movement of Spent N Reactor fuels from the Hanford K Basins near the Columbia River to Dry interim storage facility on the Hanford plateau will require repackaging the fuel in the basins into multi-canister overpacks (MCOs), drying of the fuel, transporting the contained fuel, hot conditioning, and finally interim storage. Each of these functions will be accomplished while the fuel is contained in the MCOs by several mechanisms. The principal source of hydrogenand oxygen within the MCOs is residual water from the vacuum drying and hot conditioning operations. This document assesses the Detonation Phenomena of hydrogen and oxygen in the spent fuel containers. Several process scenarios have been identified that could generate Detonation pressures that exceed the nominal 10 atmosphere design limit ofthe MCOS. Only 42 grams of radiolized water are required to establish this condition.
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Spent nuclear fuel project Detonation Phenomena of hydrogen/oxygen in spent fuel containers
1996Co-Authors: T D CooperAbstract:Movement of Spent N Reactor fuels from the Hanford K Basins near the Columbia River to Dry interim storage facility on the Hanford plateau will require repackaging the fuel in the basins into multi-canister overpacks (MCOs), drying of the fuel, transporting the contained fuel, hot conditioning, and finally interim storage. Each of these functions will be accomplished while the fuel is contained in the MCOs by several mechanisms. The principal source of hydrogenand oxygen within the MCOs is residual water from the vacuum drying and hot conditioning operations. This document assesses the Detonation Phenomena of hydrogen and oxygen in the spent fuel containers. Several process scenarios have been identified that could generate Detonation pressures that exceed the nominal 10 atmosphere design limit ofthe MCOS. Only 42 grams of radiolized water are required to establish this condition.
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snfp Detonation Phenomena of hydrogen oxygen in spent fuel containers
Other Information: PBD: 30 May 1996, 1996Co-Authors: T D CooperAbstract:Movement of spent nuclear fuels from the Hanford K Basins near the Columbia River to dry interim storage facility on the Hanford plateau will require repackaging the fuel in the basin into multi-canister overpacks (MCOs), drying of the fuel, transporting the contained fuel, hot conditioning, and finally interim storage. Each of these functions will be accomplished while the fuel is contained in the MCOs. Hydrogen and oxygen can be generated within the MCOs by several mechanisms. The principal source of hydrogen and oxygen within the MCOs is residual water from the vacuum drying and hot conditioning operations. This document assesses the Detonation Phenomena of hydrogen and oxygen in the spent fuel containers. Several process scenarios have been identified that could generate Detonation pressures that exceed the nominal 10 atmosphere design limit of the MCOs. Only 42 grams of radiolized water are required to establish this condition.
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SNFP Detonation Phenomena of hydrogen/oxygen in spent fuel containers
1996Co-Authors: T D CooperAbstract:Movement of spent nuclear fuels from the Hanford K Basins near the Columbia River to dry interim storage facility on the Hanford plateau will require repackaging the fuel in the basin into multi-canister overpacks (MCOs), drying of the fuel, transporting the contained fuel, hot conditioning, and finally interim storage. Each of these functions will be accomplished while the fuel is contained in the MCOs. Hydrogen and oxygen can be generated within the MCOs by several mechanisms. The principal source of hydrogen and oxygen within the MCOs is residual water from the vacuum drying and hot conditioning operations. This document assesses the Detonation Phenomena of hydrogen and oxygen in the spent fuel containers. Several process scenarios have been identified that could generate Detonation pressures that exceed the nominal 10 atmosphere design limit of the MCOs. Only 42 grams of radiolized water are required to establish this condition.
Melanie C. Kuckels - One of the best experts on this subject based on the ideXlab platform.
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JANNAF 19th Propulsion Systems Hazards Subcommittee Meeting
2019Co-Authors: Melanie C. Kuckels, James E. CocchiaroAbstract:This volume, the first of two volumes is a compilation of 25 unclassified/unlimited-distribution technical papers presented at the Joint Army-Navy-NASA-Air Force (JANNAF) 19th Propulsion Systems Hazards Subcommittee (PSHS) meeting held jointly with the 37th Combustion Subcommittee (CS) and 25th Airbreathing Propulsion Subcommittee (APS), and 1st Modeling and Simulation Subcommittee (MSS) meetings. The meeting was held 13-17 November 2000 at the Naval Postgraduate School and Hyatt Regency Hotel, Monterey, California. Topics covered at the PSHS meeting include: impact and thermal vulnerability of gun propellants; thermal decomposition and cookoff behavior of energetic materials; violent reaction and Detonation Phenomena of solid energetic materials subjected to shock and impact loading; and hazard classification, and insensitive munitions testing of propellants and propulsion systems.
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JANNAF 19th Propulsion Systems Hazards Subcommittee Meeting. Volume 1
2000Co-Authors: James E. Cocchiaro, Melanie C. KuckelsAbstract:Abstract : This volume, the first of two volumes is a compilation of 25 unclassified/unlimited-distribution technical papers presented at the Joint Army-Navy-NASA-Air Force (JANNAF) 19th Propulsion Systems Hazards Subcommittee (PSHS) meeting held jointly with the 37th Combustion Subcommittee (CS) and 25th Airbreathing Propulsion Subcommittee (APS), and 1st Modeling and Simulation Subcommittee (MSS) meetings. The meeting was held 13-17 November 2000 at the Naval Postgraduate School and Hyatt Regency Hotel, Monterey, California. Topics covered at the PSHS meeting include: impact and thermal vulnerability of gun propellants; thermal decomposition and cookoff behavior of energetic materials; violent reaction and Detonation Phenomena of solid energetic materials subjected to shock and impact loading; and hazard classification, and insensitive munitions testing of propellants and propulsion systems.
Melanie Rognan - One of the best experts on this subject based on the ideXlab platform.
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JANNAF 17th Propulsion Systems Hazards Subcommittee Meeting. Volume 1; Held at Raytheon Systems Company and Marriott University Park, Tucson, AZ on 7-11 December 1998
1998Co-Authors: James E. Cocchiaro, Mary T. Gannaway, Melanie RognanAbstract:Abstract : Volume I, the first of two volumes is a compilation of 16 unclassified/unlimited technical papers presented at the 17th meeting of the Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Systems Hazards Subcommittee (PSHS) held jointly with the 35th Combustion Subcommittee (CS) and Airbreathing Propulsion Subcommittee (APS). The meeting was held on 7-11 December 1998 at Raytheon Systems Company and the Marriott Hotel, Tucson, AZ. Topics covered include projectile and shaped charge jet impact vulnerability of munitions; thermal decomposition and cookoff behavior of energetic materials; damage and hot spot initiation mechanisms with energetic materials; Detonation Phenomena of solid energetic materials; and hazard classification, insensitive munitions, and propulsion systems safety.
C J Wang - One of the best experts on this subject based on the ideXlab platform.
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numerical analysis of vortex like structure induced mechanism in gaseous Detonation Phenomena
PROCEEDINGS OF THE 2ND INTERNATIONAL SYMPOSIUM ON COMPUTATIONAL MECHANICS AND THE 12TH INTERNATIONAL CONFERENCE ON THE ENHANCEMENT AND PROMOTION OF CO, 2010Co-Authors: C J WangAbstract:Two‐dimensional, time‐dependent, reactive Navier—Stokes equations involving the effects of viscosity, thermal conduction, molecular diffusion and turbulence etc. were solved to obtain a deep insight into gaseous Detonation vortex‐like structures and its induced mechanism. Detailed chemical reaction model, together with standard κ‐e turbulence model, was employed in this paper. Numerical simulation indicates that a large amount of vortex‐like structure emerges in Detonation flow field due to its intrinsic three‐dimensional structure. Vortex‐like structure can also be induced by wall geometry with an abrupt cross‐section area change. Shock wave interacts with slip line, which in turn causes the formation of vortex‐like structure. In nature, all these induce the instability of slip line, so it is the slip line instability that is the essential reason for the emergence of vortex‐like structure. Additionally, the difference of vortex‐like structure between an ordinary Detonation and a marginal Detonation was c...
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Numerical Analysis of Vortex‐like structure induced mechanism in Gaseous Detonation Phenomena
2010Co-Authors: C J WangAbstract:Two‐dimensional, time‐dependent, reactive Navier—Stokes equations involving the effects of viscosity, thermal conduction, molecular diffusion and turbulence etc. were solved to obtain a deep insight into gaseous Detonation vortex‐like structures and its induced mechanism. Detailed chemical reaction model, together with standard κ‐e turbulence model, was employed in this paper. Numerical simulation indicates that a large amount of vortex‐like structure emerges in Detonation flow field due to its intrinsic three‐dimensional structure. Vortex‐like structure can also be induced by wall geometry with an abrupt cross‐section area change. Shock wave interacts with slip line, which in turn causes the formation of vortex‐like structure. In nature, all these induce the instability of slip line, so it is the slip line instability that is the essential reason for the emergence of vortex‐like structure. Additionally, the difference of vortex‐like structure between an ordinary Detonation and a marginal Detonation was c...