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Supervisors' Foreword; Acknowledgments; Contents; Acronyms; 1 Introduction; 1.1 Background; 1.1.1 Academic Background; 1.1.2 Engineering Background; 1.2 Physical Analysis; 1.3 Questions Proposed; 1.4 Research Status; 1.4.1 Rarefied Gas Effects; 1.4.2 Nonequilibrium Real Gas Effects; 1.4.3 Coupling Interaction Between Rarefied Gas Effects and Nonequilibrium Real Gas Effects; 1.5 Content and Innovations of this Thesis; 1.5.1 Methodology; 1.5.2 Research Content; 1.5.3 Innovations of this Work; References; 2 Theoretical Modeling of Aeroheating Under Rarefied Gas Effects; 2.1 Problem Description
2.2 Analysis and Research Idea2.3 Nonlinear Heat Transfer in Hypersonic Rarefied Flows; 2.3.1 Theoretical Basis; 2.3.2 Rarefied Flow Criterion; 2.3.3 Analysis of Flow Field Structure Features; 2.3.4 Flow Regime Classification and Flow Field Structure Discussion; 2.3.5 Aeroheating Performance and Bridging Function; 2.3.6 DSMC Results and Experimental Data; 2.3.7 Extension and Discussion of the Rarefaction Criterion; 2.4 Engineering Applications; 2.5 Chapter Summary; References; 3 Theoretical Modeling of the Chemical Nonequilibrium Flow Behind a Normal Shock Wave; 3.1 Problem Description
3.2 Physical Model3.3 Dissociation-Recombination Reaction Rate Equation; 3.4 Analysis of Post-Shock Chemical Nonequilibrium Flow Features; 3.4.1 Equilibrium Degree of Dissociation; 3.4.2 Characteristic Nonequilibrium Scale; 3.4.3 Nonequilibrium Transient Process; 3.5 Engineering Applications; 3.6 Chapter Summary; References; 4 Theoretical Modeling of Aero-Heating Under Nonequilibrium Real Gas Effects; 4.1 Problem Description and Modeling; 4.2 Dissociation Nonequilibrium Flow Outside SPBL; 4.2.1 Governing Equation; 4.2.2 Explicitly Analytical Shock Mapping Relation
4.2.3 Nonequilibrium Flow Criterion and Flow Regime Classification4.2.4 Validations; 4.2.5 Discussions; 4.3 Recombination Nonequilibrium Flow Inside SPBL and Heat Transfer; 4.3.1 Governing Equation; 4.3.2 Recombination Nonequilibrium Flow Criterion; 4.3.3 Bridging Function of the Nonequilibrium SPBL Heat Transfer; 4.3.4 Features of Nonequilibrium SPBL Heat Transfer; 4.4 Discussion of Flow Similarity; 4.5 Engineering Applications; 4.6 Chapter Summary; References; 5 Conclusions and Prospect; 5.1 Conclusions; 5.2 Prospect
2.2 Analysis and Research Idea2.3 Nonlinear Heat Transfer in Hypersonic Rarefied Flows; 2.3.1 Theoretical Basis; 2.3.2 Rarefied Flow Criterion; 2.3.3 Analysis of Flow Field Structure Features; 2.3.4 Flow Regime Classification and Flow Field Structure Discussion; 2.3.5 Aeroheating Performance and Bridging Function; 2.3.6 DSMC Results and Experimental Data; 2.3.7 Extension and Discussion of the Rarefaction Criterion; 2.4 Engineering Applications; 2.5 Chapter Summary; References; 3 Theoretical Modeling of the Chemical Nonequilibrium Flow Behind a Normal Shock Wave; 3.1 Problem Description
3.2 Physical Model3.3 Dissociation-Recombination Reaction Rate Equation; 3.4 Analysis of Post-Shock Chemical Nonequilibrium Flow Features; 3.4.1 Equilibrium Degree of Dissociation; 3.4.2 Characteristic Nonequilibrium Scale; 3.4.3 Nonequilibrium Transient Process; 3.5 Engineering Applications; 3.6 Chapter Summary; References; 4 Theoretical Modeling of Aero-Heating Under Nonequilibrium Real Gas Effects; 4.1 Problem Description and Modeling; 4.2 Dissociation Nonequilibrium Flow Outside SPBL; 4.2.1 Governing Equation; 4.2.2 Explicitly Analytical Shock Mapping Relation
4.2.3 Nonequilibrium Flow Criterion and Flow Regime Classification4.2.4 Validations; 4.2.5 Discussions; 4.3 Recombination Nonequilibrium Flow Inside SPBL and Heat Transfer; 4.3.1 Governing Equation; 4.3.2 Recombination Nonequilibrium Flow Criterion; 4.3.3 Bridging Function of the Nonequilibrium SPBL Heat Transfer; 4.3.4 Features of Nonequilibrium SPBL Heat Transfer; 4.4 Discussion of Flow Similarity; 4.5 Engineering Applications; 4.6 Chapter Summary; References; 5 Conclusions and Prospect; 5.1 Conclusions; 5.2 Prospect