16.100 Aerodynamics, Fall 2002

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 bou...

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Bibliographic Details
Main Author:	Darmofal, David L.
Other Authors:	Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Format:	Learning Object
Language:	en-US
Published:	2002
Subjects:	aerodynamics airflow air body aircraft aerodynamic modes aero forces CFD aerodynamic analysis lift potential flows supersonic subsonic panel method vortex lattice method boudary layer transition turbulence inviscid viscous euler navier-stokes wind tunnel flow similarity non-dimensional mach number reynolds number integral momentum airfoil stall friction drag drag induced drag wave drag pressure drag fluid element shear strain normal strain vorticity divergence substantial derviative laminar displacement thickness momentum thickness skin friction separation velocity profile 2-d panel 3-d vortex thin airfoil lifting line aspect ratio twist camber wing loading roll moments finite volume approximation shocks expansion fans shock-expansion theory transonic critical mach number wing sweep Kutta condition team project blended-wing-body computational fluid dynamics Incompressible Aerodynamics
Online Access:	http://hdl.handle.net/1721.1/36884

Internet

http://hdl.handle.net/1721.1/36884

16.100 Aerodynamics, Fall 2002

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