Fluidic Injection Scenarios for Shock Pattern Manipulation in Exhausts
Author:
Affiliation:
1. University of Cambridge, Cambridge, England CB3 0DY, United Kingdom
2. Royal Institute of Technology, 10044 Stockholm, Sweden
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057537
Reference2 articles.
1. Understanding How Chevrons Modify Noise in Supersonic Jet with Flight Effects
2. Acoustics and Thrust of Quiet Separate-Flow High-Bypass-Ratio Nozzles
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