System energy benefit using co-flow jet active separation control for a serpentine duct-Reference-Cited by-同舟云学术

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System energy benefit using co-flow jet active separation control for a serpentine duct

Published:2022-09 Issue: Volume:128 Page:107746
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xu Kewei^ORCID,Zha Gecheng^ORCID

Funder

University of Miami

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference52 articles.

1. Mitigation of serpentine duct flow distortion using coflow jet active flow control;Xu,2020

2. Blended wing body systems studies: boundary layer ingestion inlets with active flow control;Geiselhart,2003

3. Blended wing body (bwb) boundary layer ingestion (bli) inlet configuration and system studies;Kawai,2006

4. Aerodynamic flowfield control technologies for highly integrated airframe propulsion flowpaths;Miller,2004

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1. Design and aerodynamic stability improvement study of a non-axisymmetric stator fan in a distorted insertion plate configuration;Aerospace Science and Technology;2024-12

2. Wing design optimization and stall analysis with Co-flow Jet active control;Physics of Fluids;2024-04-01

3. Behavior of flow distortion within a boundary layer ingestion inlet;Aerospace Science and Technology;2024-03

4. Improved Delayed Detached Eddy Simulation of Co-Flow Jet Flow Control in Extreme Adverse Pressure Gradients;AIAA SCITECH 2024 Forum;2024-01-04

5. Distortion elimination for serpentine duct at various Mach numbers using co-flow jet active flow control;Aerospace Science and Technology;2024-01

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