Aeronautical and Space Sciences Japan
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
 
Acoustic Wind Tunnel Test with 18% Scale Half-span Model of ‘Hisho’
Yuzuru YOKOKAWA
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Keywords: Airframe Noise, Flap, Noise Reduction Devices, Wind Tunnel Experiment, Flight Demonstration
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2020 Volume 68 Issue 5 Pages 154-160

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[in Japanese]
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© 2020 The Japan Society for Aeronautical and Space Sciences
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