Toward a Passive Control Strategy for a Supersonic Multi-Stream Flow using Resolvent Analysis-Reference-Cited by-同舟云学术

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Toward a Passive Control Strategy for a Supersonic Multi-Stream Flow using Resolvent Analysis

Published:2021-01-04 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2021 Forum
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Author:

Doshi Parshwanath S.¹,Ranjan Rajesh¹,Liu Qiong¹,Gist Emma D.²,Gaitonde Datta V.¹,Glauser Mark N.²

Affiliation:

1. Ohio State University

2. Syracuse University

Publisher

American Institute of Aeronautics and Astronautics

Reference53 articles.

1. Kyprianidis, K. G. “Multi-disciplinary conceptual design of future jet engine systems,” Ph.D. thesis,2010.

2. Simmons, R. J. “Design and control of a variable geometry turbofan with and independently modulated third stream,” Ph.D. thesis,The Ohio State University, 2009.

3. The nonaxisymmetric nozzle - It is for real<149>fighter aircraft performance viewpoint

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1. Schlieren-Based Analysis of Supersonic Multistream Control Using Data-Driven and Filtering Techniques;AIAA Journal;2024-09-02

2. Responses to disturbance of supersonic shear layer: Input-output analysis;Physical Review Fluids;2024-08-12

3. Passive Control of Supersonic Shear Layer in Rectangular Multistream Jet;AIAA Journal;2022-10

4. Global and local modal characteristics of supersonic open cavity flows;Physics of Fluids;2022-03

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