Advanced methods and concepts for aerodynamic analysis of aircraft, including airfoil theory, finite wing theory, far-field and Trefftz-plane analysis, two-dimensional laminar and turbulent boundary layers, and laminar-to-turbulent transition. Focus is on developing both (a) a deep understanding of the fundamentals and (b) the ability to estimate aerodynamic performance using fast computational methods appropriate for conceptual and preliminary aircraft design. We also explore the connection, through relevant examples, between aerodynamic theories and practical implications of aerodynamic performance and stability and control. Weekly assignments may require the use of a suitable programming language (MATLAB, Python, or C/C++ recommended).
3 units · Letter (ABCD/NP)
Advanced methods and concepts for aerodynamic analysis of aircraft, including airfoil theory, finite wing theory, far-field and Trefftz-plane analysis, two-dimensional laminar and turbulent boundary layers, and laminar-to-turbulent transition. Focus is on developing both (a) a deep understanding of the fundamentals and (b) the ability to estimate aerodynamic performance using fast computational methods appropriate for conceptual and preliminary aircraft design. We also explore the connection, through relevant examples, between aerodynamic theories and practical implications of aerodynamic performance and stability and control. Weekly assignments may require the use of a suitable programming language (MATLAB, Python, or C/C++ recommended).
Offered in Winter 2027 at Stanford University.