ubuntu2404
\contentsline {section}{\numberline {1}Introduction}{2}{section.1}%
\contentsline {section}{\numberline {2}Aerodynamics Analysis}{2}{section.2}%
\contentsline {subsection}{\numberline {2.1}NACA Airfoil Geometry}{2}{subsection.2.1}%
\contentsline {subsection}{\numberline {2.2}Aerodynamic Performance Analysis}{2}{subsection.2.2}%
\contentsline {section}{\numberline {3}CFD Analysis Fundamentals}{3}{section.3}%
\contentsline {subsection}{\numberline {3.1}Governing Equations}{3}{subsection.3.1}%
\contentsline {subsection}{\numberline {3.2}Dimensionless Parameters}{3}{subsection.3.2}%
\contentsline {section}{\numberline {4}Propulsion Analysis}{3}{section.4}%
\contentsline {subsection}{\numberline {4.1}Turbojet Engine Performance}{3}{subsection.4.1}%
\contentsline {section}{\numberline {5}Flight Dynamics}{4}{section.5}%
\contentsline {subsection}{\numberline {5.1}Aircraft Stability Analysis}{4}{subsection.5.1}%
\contentsline {section}{\numberline {6}Computational Methods}{5}{section.6}%
\contentsline {subsection}{\numberline {6.1}Finite Difference Discretization}{5}{subsection.6.1}%
\contentsline {section}{\numberline {7}Conclusion}{6}{section.7}%
\contentsline {section}{\numberline {8}References}{6}{section.8}%