Aerodynamic/Acoustic Analysis for Main Rotor and Tail Rotor of Helicopter-Reference-Cited by-同舟云学术

Aerodynamic/Acoustic Analysis for Main Rotor and Tail Rotor of Helicopter

Published:2008 Issue:171 Volume:51 Page:28-36
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

YANG Choongmo¹,AOYAMA Takashi¹,KONDO Natsuki¹,SAITO Shigeru¹

Affiliation:

1. Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/51/171/51_171_28/_pdf

Reference21 articles.

1. 1) White, R. P. Jr.: The Status of Rotor Noise Technology: One Man’s Opinion, NASA Center for AeroSpace Information (CASI), 1978.

2. 2) Chou, S.-T.: A Study of Rotor Broadband Noise Mechanism and Helicopter Tail Rotor Noise, NASA-CR-177565, 1990.

3. 3) Martin, R. M.: Acoustic Test of a Model Rotor and Tail Rotor: Results for the Isolated Rotor and Combined Configuration, NASA-TM-101550, 1989.

4. 4) Balch, D. T. and Lombardi, J.: Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interaction in Hover. Volume 1. Text and Figures, NASA-CR-177336-VOL-1, 1985.

5. 5) Balch, D. T. and Lombardi, J.: Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interaction in Hover. Volume 2. Run Log and Tabulated Data, NASA-CR-177336-VOL-2, 1985.

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