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Aerodynamics, Fall 2005
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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.

Subject:
Engineering
Material Type:
Full Course
Provider:
MIT
Provider Set:
MIT OpenCourseWare
Author:
Darmofal, David
Date Added:
01/01/2005
Computational Thinking Concepts Guide from Google
Conditional Remix & Share Permitted
CC BY-NC-SA
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In this guide you will find eleven terms and definitions for Computational Thinking (CT) concepts. These concepts can be incorporated into existing lesson plans, projects, and demonstrations in order to infuse CT into any disciplinary subject.

The original copy of this information was created by Google and shared at https://docs.google.com/document/d/1i0wg-BMG3TdwsShAyH_0Z1xpFnpVcMvpYJceHGWex_c/edit. The only change made has been the format of the document. All information is exactly the same.

Subject:
Architecture and Design
Computer Science
Engineering
Information Science
Mathematics
Material Type:
Reading
Author:
Gina Loveless
Date Added:
08/28/2020