Distortion elimination for serpentine duct at various Mach numbers using co-flow jet active flow control-Reference-Cited by-同舟云学术

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Distortion elimination for serpentine duct at various Mach numbers using co-flow jet active flow control

Published:2024-01 Issue: Volume:144 Page:108776
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xu Kewei,Zha Gecheng^ORCID

Funder

University of Miami

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference56 articles.

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

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

3. Aircraft Engine Design;Mattingly,2002

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

5. An experimental investigation of s-duct flow control using arrays of low-profile vortex generators;Reichert,1993

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