This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic …
This course extends fluid mechanic concepts from Unified Engineering to the aerodynamic performance of wings and bodies in sub/supersonic regimes. 16.100 generally has four components: subsonic potential flows, including source/vortex panel methods; viscous flows, including laminar and turbulent boundary layers; aerodynamics of airfoils and wings, including thin airfoil theory, lifting line theory, and panel method/interacting boundary layer methods; and supersonic and hypersonic airfoil theory. Course material varies each year depending upon the focus of the design problem.
This course is about the mathematics that is most widely used in …
This course is about the mathematics that is most widely used in the mechanical engineering core subjects: An introduction to linear algebra and ordinary differential equations (ODEs), including general numerical approaches to solving systems of equations.
Derivation of Euler's formula from a Taylor series expansion of the expontential …
Derivation of Euler's formula from a Taylor series expansion of the expontential function for a complex argument.Derivation of the multiple angle trig identities for sine and cosine using the Binaomial theorem and Euler's formula.
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