This video takes a look at a smoke probe visualization of airflow over a model of an F16 aircraft. The visualization is created in the Wright Brothers Wind Tunnel. Two flow regimes are shown. The first is a low angle of attack visualization, where the flow field appears steady, or independent of time. The second flow regime has the model at a high angle of attack. In this case, the flow appears unsteady, which shows that the flow field has a time dependence. Prof. Dave Darmofal ends the demonstration by discussing how these visualizations are used in engineering.
After watching this video students will be able to:
Funding provided by the Singapore University of Technology and Design (SUTD)
Developed by the Teaching and Learning Laboratory (TLL) at MIT for SUTD
MIT © 2012
During the video, students will: