16.100 Aerodynamics
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....
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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.
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Material Type:
Online Course
Date Added to MERLOT:
October 20, 2011
Date Modified in MERLOT:
October 30, 2013
Submitter:
Sorel
Reisman
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Reviewed by members of Editorial board for inclusion in MERLOT.Editor ReviewVery good quality; in queue to be peer reviewedavg:
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English
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This work is licensed under a Attribution-NonCommercial-ShareAlike 3.0 United States
This work is licensed under a Attribution-NonCommercial-ShareAlike 3.0 United States
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