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|a QD516
|b .I58 1989eb
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|a 629.1 s
|a 541.3/61
|2 20
|
| 049 |
|
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|a UAMI
|
| 111 |
2 |
|
|a International Colloquium on Dynamics of Explosions and Reactive Systems
|n (12th :
|d 1989 :
|c Ann Arbor, Mich.)
|
| 245 |
1 |
0 |
|a Dynamics of detonations and explosions :
|b explosion phenomena /
|c edited by A.L. Kuhl [and others].
|
| 260 |
|
|
|a Washington, D.C. :
|b American Institute of Aeronautics and Astronautics,
|c ©1991.
|
| 300 |
|
|
|a 1 online resource (xx, 408 pages) :
|b illustrations
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia
|
| 338 |
|
|
|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a Progress in astronautics and aeronautics ;
|v v. 134
|
| 500 |
|
|
|a "Technical papers presented from the Twelfth International Colloquium on Dynamics of Explosions and Reactive Systems, Ann Arbor, Michigan, July 1989, and subsequently revised for this volume."
|
| 504 |
|
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|a Includes bibliographical references and index.
|
| 505 |
0 |
|
|a Cover -- Title -- Copyright -- Table of Contents -- Preface -- Chapter I. Vapor Cloud Explosions -- Scaling of Vapor Cloud Explosions After Turbulent Jet Release -- Effect of Asymmetric Ignition on the Vapor Cloud Spatial Blast -- Experimental Investigation Concerning the Influenceof Turbulence on the Flame Front Velocity of FuelGas-Air Mixture Deflagrations -- Mechanism of Flame Acceleration Alonga Tube With Obstacles -- Explosion in a Vented Vessel Connected to a Duct
|
| 505 |
8 |
|
|a Modelization and Validation Tests of the Dischargein Air of a Vessel Pressurized by a Flammable GasApplicability of a Chemical-Equilibrium Modelto Explosion Products -- Inverse Numerical Process for Inlet ConditionsCalculus from Experimental Front Determination -- Chapter II. Blast Wave Reflections and Interactions -- Reflection of Shock and Explosion Waves from Surfaces Covered with Layers of Polyurethane Foam -- Simulating the Impact Made by a Shock Wave on aBody Surrounded by a Layer of Hot or Cold Gas -- Turbulent Wall Jet in a Mach Reflection Flow
|
| 505 |
8 |
|
|a Numerical Simulation of the Change in theSupersonic Flow Past a Body Produced by Switchingon a Nearby Heat SourceShock Waves Produced by Reflected Detonations -- Spherical Wave Interaction with a Liquid-AirInterface: Analysis of the Holographic Results -- Formation of Zones with High ParticleConcentrations in Dusty Gas -- Chapter III. Vapor Explosions -- Shock Waves From Vapor Explosion in aShock Tube -- Dynamics of Explosive Interactions Between MoltenTin and Water in Stratified Geometry -- Steam Explosion Studies with Molten Iron-AluminaGenerated by Thermite Reactions
|
| 505 |
8 |
|
|a Application of the Integrated Fuel-CoolantInteraction Code to a FITS-TypePouring Mode ExperimentMultiphase Physical Explosion ModelingUsing the CULDESAC Code -- Author Index
|
| 590 |
|
|
|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 650 |
|
0 |
|a Explosions
|v Congresses.
|
| 650 |
|
0 |
|a Gas dynamics
|v Congresses.
|
| 650 |
|
6 |
|a Explosions
|v Congrès.
|
| 650 |
|
6 |
|a Dynamique des gaz
|v Congrès.
|
| 650 |
|
7 |
|a Explosions
|2 fast
|
| 650 |
|
7 |
|a Gas dynamics
|2 fast
|
| 655 |
|
7 |
|a Conference papers and proceedings
|2 fast
|
| 700 |
1 |
|
|a Kuhl, A. L.
|
| 710 |
2 |
|
|a American Institute of Aeronautics and Astronautics.
|
| 776 |
0 |
8 |
|i Print version:
|a International Colloquium on Dynamics of Explosions and Reactive Systems (12th : 1989 : Ann Arbor, Mich.).
|t Dynamics of detonations and explosions.
|d Washington, D.C. : American Institute of Aeronautics and Astronautics, ©1991
|w (DLC) 91007934
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 134.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111558
|z Texto completo
|
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