Wall Interference Correction Method for Kevlar Wall Test Section
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA), Mitaka, Tokyo 183-0015, Japan
2. IHI Aerospace Engineering, Mitaka, Tokyo 183-0015, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Design and Characterization of a High-Speed Subsonic Aeroacoustic Wind Tunnel
2. Design of an Aeroacoustic Wind Tunnel Facility at the University of Bristol
3. Development and Testing of a Novel Acoustic Wind Tunnel Concept
4. The Kevlar-walled anechoic wind tunnel
5. Aerodynamic/Aeroacoustic testing in Anechoic Closed Test Sections of Low-Speed Wind Tunnels
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1. Experimental Investigation of the Influence of Aerodynamic Loading on the Transmission Loss Through Kevlar Membranes;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
2. Blending of Reynolds Stress Transport Model and γ Transition Model;AIAA Journal;2023-02
3. Fluid–Structure Interaction Modeling of Flowfields Within Kevlar-Walled Wind Tunnels;Journal of Aircraft;2022-09
4. Investigating the Aeroacoustic Properties of Porous Fabrics;AIAA Journal;2022-06
5. Propagation characteristics of laser-induced acoustic sources in hybrid anechoic wind tunnels;Journal of Sound and Vibration;2021-10
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