Parametric Testing of Chevrons on Single Flow Hot Jets

By J. Bridges, Clifford A. Brown. 2004

364 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/c553151f768de8a00290cc6d2b87d38690e41ba7

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. Tim Colonius
2. G. Butler
3. M. Alkislar
4. Anjaneyulu Krothapalli
5. Takao Suzuki
6. P. Jordan
7. Christophe Bogey
8. Christophe Bailly

In Computational Mechanics

1. Tim Colonius
2. G. Butler
3. M. Alkislar
4. Anjaneyulu Krothapalli
5. Takao Suzuki
6. Christophe Bogey
7. Christophe Bailly
8. P. Jordan

In Environmental Engineering

1. M. Alkislar
2. Anjaneyulu Krothapalli
3. Tim Colonius
4. Takao Suzuki
5. P. Jordan
6. Aaron Towne
7. Oliver T. Schmidt

Citations in the corpus

• The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet (2007, background): “With the continuing emphasis on noise reduction techniques that do not significantly interfere with the flow, chevron nozzles have received much attention (Bridges, Wernet & Brown 2003; Saiyed, Mikkelsen & Bridges 2003; Bridges & Brown 2004).”
• Instability waves in a subsonic round jet detected using a near-field phased microphone array (2006, methodology): “Subsequently, we describe the experimental facilities, test conditions and final array design for the laboratory-scale jets (Re 105) based on mean-flow data from particle image velocimetry (PIV) by Bridges & Wernet (2003) and Bridges & Brown (2004) in § 4.”