Splitter Plate Edge Effects in a Supersonic Multi-stream Nozzle-Reference-Cited by-同舟云学术

Splitter Plate Edge Effects in a Supersonic Multi-stream Nozzle

Published:2018-07-08 Issue: Volume: Page:
ISSN:
Container-title:2018 Joint Propulsion Conference
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Author:

Ruscher Christopher J.¹,Gogineni Sivaram¹,Ferrill Thomas²

Affiliation:

1. Spectral Energies, LLC

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4745

Reference46 articles.

1. Simmons, R. J., Design and Control of a Variable Geometry Turbofan with an Independently Modulated Third Stream, Ph.D. thesis,The Ohio State University, 2009.

2. Aeroacoustics of Three-Stream High-Speed Jets from Coaxial and Asymmetric Nozzles

3. Measurements and Predictions of the Noise from Three-Stream Jets

4. Simple Scaling Of Multi-Stream Jet Plumes For Aeroacoustic Modeling

5. Characterization of Three-stream Jets

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