Effect of orifice shape in synthetic jet based impingement cooling

By M. Chaudhari, Bhalchandra P. Puranik, Amit Agrawal. 2010

161 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/2e8c110ecaedf9861fb8be18be72b85212d34060

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. Tim Persoons
3. Alan McGuinn
4. Amit Agrawal
5. Bhalchandra P. Puranik

In Computational Mechanics

1. Tim Persoons
2. Alan McGuinn
3. D. Murray
4. Bhalchandra P. Puranik
5. Amit Agrawal
6. Lounes Tadrist
7. John Richard Thome

In Mechanical Engineering

1. Tim Persoons
2. Alan McGuinn
3. D. Murray
4. Amit Agrawal
5. Lounes Tadrist
6. Bhalchandra P. Puranik
7. John Richard Thome

Citations in the corpus

• An overview of heat transfer enhancement methods and new perspectives: Focus on active methods using electroactive materials (2013, background): “[168] studied the effect of orifice shape on heat transfer enhancement using a synthetic jet.”
• A general correlation for the stagnation point Nusselt number of an axisymmetric impinging synthetic jet (2011, background): “The synthetic jet Nu0 correlations available in the literature [18,22,23] are listed in Table 2, and are compared to the correlation obtained in the present study in Fig.”
• A numerical investigation of effects of cavity and orifice parameters on the characteristics of a synthetic jet flow (2011, background): “Synthetic jet and these alternate designs can be used for cooling/drying applications [15–17].”