Experimental study of the formation and scaling of a round synthetic jet

By J. Shuster, Douglas R. Smith. 2007

195 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/3b6dd62a00db66baff4f61363a6c430fa26ee6ad

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. D. Murray
2. Lihao Feng
3. Jinjun Wang
4. P. Valiorgue
5. Tim Persoons
6. Alan McGuinn

In Computational Mechanics

1. Tim Persoons
2. Alan McGuinn
3. P. Valiorgue
4. D. Murray
5. Lihao Feng
6. Jinjun Wang

Citations in the corpus

• Circular cylinder vortex-synchronization control with a synthetic jet positioned at the rear stagnation point (2010, background): “In recent decades, the synthetic-jet flow-control technique has drawn much attention because of its great advantages (Smith & Glezer 1998; Shuster & Smith 2007).”
• Heat transfer mechanisms in an impinging synthetic jet for a small jet-to-surface spacing (2009, methodology): “For a free synthetic jet flow, Shuster and Smith [2] show that the distance 180 traveled by the propagating vortex scales with the stroke length.”
• A general correlation for the stagnation point Nusselt number of an axisymmetric impinging synthetic jet (2011, background): “For flow control applications, Shuster and Smith [15] concluded that low stroke length regimes should be avoided to maximize the far field momentum flux of a synthetic jet.”