Aeroacoustic environment of an advanced STOVL aircraft in hover

Author:

WLEZIEN RICHARD1,FERRARO PETER2

Affiliation:

1. Illinois Institute of Technology, Chicago

2. McDonnell Aircraft Co., Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. L Fig.3 Configurationfor near-fieldacousticmeasure

2. wing loads are 4-6 dB greater than those for the round nozzles. At largerhn the fuselageloads areof the same orderorlowerthan thatfortheothernozzles,butthewing remains greater. Thesedifferencesarea consequenceof the strong lateral screech coupling observed for this configuration. The intense screech and impingement tones tend to increase the fuselage loading in regions away from the fountain impingementzone. The wing loadingpattern isconsistentwith the acoustic directivity of therectangularplumeflappingmode.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Aeroacoustics of Twin Supersonic Jets: A Review;International Journal of Aeroacoustics;2012-12

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