Passive Control of Supersonic Shear Layer in Rectangular Multistream Jet-Reference-Cited by-同舟云学术

Passive Control of Supersonic Shear Layer in Rectangular Multistream Jet

Published:2022-10 Issue:10 Volume:60 Page:5692-5706
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Doshi Parshwanath S.^ORCID,Gaitonde Datta V.,Gist Emma D.,Glauser Mark N.

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J061592

Reference54 articles.

1. KyprianidisK. G. “Multi-Disciplinary Conceptual Design of Future Jet Engine Systems,” Ph.D. Dissertation, Cranfield Univ., Bedford, U.K. 2010.

2. SimmonsR. J. “Design and Control of a Variable Geometry Turbofan with and Independently Modulated Third Stream,” Ph.D. Dissertation, The Ohio State Univ., Columbus, OH, 2009.

3. Directional Suppression of Noise from a High-Speed Jet

4. MagstadtA. S. “Investigating the Structures of Turbulence in a Multi-Stream, Rectangular, Supersonic Jet,” Ph.D. Dissertation, Syracuse Univ., Syracuse, New York, 2017.

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