An Interpretable Internet Based Multimedia Authorware that Facilitates a Collaborative Learning Environment

Not Available We propose a proof of concept demonstration of micro-balloon vortex generators and micromachined hot film sensor arrays for active control of flow separation. This program is the first step toward the development of conformal micro-balloon vg appliques. Appliques fabricated with co-located microsensors and balloon vg's will provide a revolutionary closed loop, seamless flow control system applicable to existing and future aircraft to enhance aerodynamic performance. Future weapon systems will be realized only through development of aircraft vehicle technologies that significantly and affordably improve system-level warfighting capability. To address these challenges, the team has researched revolutionary concepts for flow field cohtrol in airframe and propulsion systems. The team has demonstrated an ability to manage large-scale flow propulsion systems. The team has demonstrated an ability to manage large-scale flow behavior through small-scale actuation, particularly in regions of high receptivity and instability involving flow separation and attachment and areas within the boundary layer.