Multi-Objective Aeroacoustic Design Exploration of Launch-Pad Flame Deflector Using Large-Eddy Simulation
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33420
Reference34 articles.
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4. Plate-Angle Effects on Acoustic Waves from Supersonic Jets Impinging on Inclined Plates
5. Generation and Propagation of Pressure Waves from H-IIA Launch Vehicle at Lift-Off
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