Design and Evaluation of a Low-Noise Helicopter Blade-Reference-Cited by-同舟云学术

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Design and Evaluation of a Low-Noise Helicopter Blade

Published:2003 Issue:592 Volume:51 Page:198-206
ISSN:1344-6460
Container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:ja
Short-container-title:JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

Kondo Natsuki,Tsujiuchi Tomoka,Murashige Atsushi,Nishimura Hiroki,Aoki Makoto,Tsuchihashi Akihiko,Yamakawa Eiichi,Aoyama Takashi,Saito Shigeru

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/jjsass/51/592/51_592_198/_pdf

Reference15 articles.

1. Rotor blade–vortex interaction noise

2. 3) Philippe, J. J. and Vuillet, A.: Aerodynamic Design of Advanced Rotors with New Tip Shapes, 39th Annual Forum of the American Helicopter Society, St. Louis, Missouri, 1983.

3. 4) Marze, H. J. and Philippe, J. J.: A Quiet Helicopter—A Research Programme Today—A Reality Tomorrow, 20th European Rotorcraft Forum, 1994.

4. 5) Perry, F. J.: Aerodynamics of the Helicopter World Speed Record, 43th Annual Forum of the American Helicopter Society, 1987.

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