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|a TL574.A45
|b D84 2013eb
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|a 629.4/152
|2 23
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|a UAMI
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|a Duffa, Georges,
|e author.
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|a Ablative thermal protection systems modeling /
|c Georges Duffa.
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|a Reston, Virginia :
|b American Institute of Aeronautics and Astronautics, Inc.,
|c [2013]
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|c ©2013
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300 |
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|a 1 online resource (473 pages) :
|b illustrations
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336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a AIAA education series
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|a Includes bibliographical references and index.
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|a Print version record.
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|a This book explains the history of ablative materials and looks into the future of its design process. Topics include: modeling based on small physics scales; thermodynamics and transport properties; gas kinetics; radiative transfer; physical and chemical reactions (homogeneous and heterogeneous); fluid mechanics and effects of turbulence on physical matter; transport properties approximation; equilibrium thermodynamics in variable elemental medium; ablation of glassy materials; roughness setup and effects; and radiative transfer in materials. The objective of this book is to develop physical skills in the key scientific areas applied to the modeling of thermal protection. --
|c Edited summary from book.
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|a CONTENTS -- PREFACE -- ACKNOWLEDGMENTS -- NOMENCLATURE -- Chapter 1 Thermal Protection System Conception -- 1.1 Planetary Reentry -- 1.2 Orders of Magnitude -- 1.3 Major Classes of Materials for Thermal Protection Systems -- 1.4 Physical Problems -- Chapter 2 Conservation Laws for a Multispecies Gaseous Medium -- 2.1 Introduction -- 2.2 Conservation Laws -- 2.3 Diffusion in Neutral Medium -- 2.4 Diffusion in Weakly Charged Media -- 2.5 Calculation of Transport Coefficients -- 2.6 Medium in Thermodynamic Nonequilibrium
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|a Chapter 3 Elementary Chemical Reactions Modeling3.1 Gaseous Reactions -- 3.2 Heterogeneous Reactions -- 3.3 Relationship Between Homogeneous and Heterogeneous Reactions -- Chapter 4 Approximate Methods -- 4.1 Introduction -- 4.2 Reactive Laminar Boundary Layers -- 4.3 Injection (Blowing or Blocking) Coefficient -- 4.4 The Couette Problem Analogy -- 4.5 Approximate Calculation of Stagnation Point Heat Flux -- 4.6 Mass and Energy Balance at Wall -- 4.7 Steady State Ablation -- Chapter 5 Ablation of Carbon -- 5.1 Oxidation -- 5.2 Reactions with Nitrogen
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|a 5.3 Sublimation5.4 Relations of Dependence -- 5.5 Reaction Kinetics -- 5.6 Homogeneous Reactions -- 5.7 Example: Homogeneous Medium -- 5.8 Partition of Energy -- 5.9 Relation Between Incident Flux and Ablation -- 5.10 Precision of the Ablation Model -- 5.11 Example of Calculation: A Test with Constant Upstream Conditions -- Chapter 6 Roughness Formation -- 6.1 General Considerations -- 6.2 Scales of the Problem -- 6.3 Reactivity of a Composite Material -- 6.4 Roughness Formation -- 6.5 Applications -- Chapter 7 Turbulence and Laminar� Turbulent Transition
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|a 7.1 Coupling Between Turbulence and Surface State7.2 Nonlocal Effects of Turbulence -- 7.3 Coupling Between Turbulence and Chemical Reactions -- 7.4 Laminar�Turbulent Transition -- Chapter 8 Pyrolysis and Pyrolyzable Materials -- 8.1 A Simple Example: PTFE -- 8.2 Phenolic Resin -- 8.3 The General Model -- 8.4 The Different Levels of Solutions -- 8.5 Transport Properties -- 8.6 Application Example -- 8.7 Ablation of Carbon Phenolics -- Chapter 9 Materials Developing a Liquid Layer -- 9.1 Hydrodynamics of the Liquid Layer -- 9.2 Silica�Resin Materials
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|a 9.1 Hydrodynamics of the Liquid Layer9.2 Silica�Resin Materials -- Chapter 10 Radiation -- 10.1 Introduction -- 10.2 Radiative Transfer Equation -- 10.3 Effects of Coupling Between Flow and Radiation -- 10.4 Radiation in Porous Media -- Chapter 11 Erosion by Particle Impact -- 11.1 Introduction: Phenomenology -- 11.2 Atmospheres -- 11.3 Effect of Flow on the Particles -- 11.4 Effect of Particles on the Flow -- 11.5 Particle�Wall Interaction -- 11.6 Coupling with Ablation -- 11.7 Discussion -- Chapter 12 Testing and Specific Test Facilities
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590 |
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
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650 |
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|a Ablation (Aerothermodynamics)
|x Mathematical models.
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650 |
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6 |
|a Ablation (Aérothermodynamique)
|x Modèles mathématiques.
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650 |
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|a Ablation (Aerothermodynamics)
|x Mathematical models
|2 fast
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|a American Institute of Aeronautics and Astronautics,
|e contributor.
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758 |
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|i has work:
|a Ablative thermal protection systems modeling (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGMMy4ckjjKDmfXb9r7p8y
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
776 |
0 |
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|i Print version:
|a Duffa, Georges.
|t Ablative thermal protection systems modeling.
|d Reston, Virginia : American Institute of Aeronautics and Astronautics, Inc., [2013]
|h xxviii, 431 pages ; 24 cm.
|k AIAA education series
|z 9781624101717
|w (DLC) 10931744
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830 |
|
0 |
|a AIAA education series.
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856 |
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|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111704
|z Texto completo
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