Melboue, Florida, Institute of Technology, 2000. 157 р.
Doctor of Philosophy in Aerospace Engineering
1. Introduction
A Brief History
Aerodynamic Overview
Literature Review
Motivation and Objective
2. Solution Overview
Physical System
Mathematical Model
Computational Method
The TVD Concept
3. Preliminary Analysis
Equations for Inviscid Flow
Eigensystem Analysis
Eigenvalues and Right Eigenvectors
Left Eigenvectors
Eigensystem for 2-D Flow
Interpretation of Results
The Shock Tube Problem
Analytical Solution
Numerical Solution
ROE Scheme
TVD Scheme
ULT Scheme
4. Solution Detail
Equations for Viscous Flow (FNS)
Curvilinear Coordinate System
Coordinate Transformation
Finite Volume Approximation
Discretization Scheme
Boundary Conditions
Surface Boundary
Outer Boundary
Initial Condition
Boundary Layer Resolution
Integration Time Step
Aerodynamic Coefficients
5. Results
Flow Field
Boundary Layer
Surface Forces
Aerodynamic Data
Conclusion
References
Appendix A
Appendix B
Appendix C
Doctor of Philosophy in Aerospace Engineering
1. Introduction
A Brief History
Aerodynamic Overview
Literature Review
Motivation and Objective
2. Solution Overview
Physical System
Mathematical Model
Computational Method
The TVD Concept
3. Preliminary Analysis
Equations for Inviscid Flow
Eigensystem Analysis
Eigenvalues and Right Eigenvectors
Left Eigenvectors
Eigensystem for 2-D Flow
Interpretation of Results
The Shock Tube Problem
Analytical Solution
Numerical Solution
ROE Scheme
TVD Scheme
ULT Scheme
4. Solution Detail
Equations for Viscous Flow (FNS)
Curvilinear Coordinate System
Coordinate Transformation
Finite Volume Approximation
Discretization Scheme
Boundary Conditions
Surface Boundary
Outer Boundary
Initial Condition
Boundary Layer Resolution
Integration Time Step
Aerodynamic Coefficients
5. Results
Flow Field
Boundary Layer
Surface Forces
Aerodynamic Data
Conclusion
References
Appendix A
Appendix B
Appendix C