Comprehensive Study on Tip Vortex with Lateral Jet Flow-Reference-Cited by-同舟云学术

Comprehensive Study on Tip Vortex with Lateral Jet Flow

Published:2003 Issue:151 Volume:46 Page:7-16
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,Baek Jehyun¹,Saito Shigeru²,Aoyama Takashi²

Affiliation:

1. Pohang University of Science and Technology

2. National Aerospace Laboratory

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/46/151/46_151_7/_pdf

Reference18 articles.

1. 1) Brook, T. F., Jolly, J. R. and Marcolini, M. A.: Helicopter Main-Rotor Noise, NASA Technical Paper 2825, 1988.

2. 2) Jacklin, S. A. and Nguyen, K. Q.: Full-Scale Wind Tunnel Test of a Helicopter Individual Blade Control System, 50th Annual Forum of the American Helicopter Society, 1994.

3. 3) Splettstoesser, W., Kube, R., Wagner, W., Seelhorst, U., Boutier, A., Micheli, F., Mercker, E. and Pengel, K.: Key Results from a Higher Harmonic Control Aeroacoustics Rotor Test (HART), J. Am. Helicopter Soc., 42 (1998), pp. 58–78.

4. 4) Hassan, A. A., Charles, B. D., Tadgahighi, H. and Sankar, L. N.: Blade-Mounted Trailing Edge Flap Control for BVI Noise Reduction, NASA Contractor Report 4426, 1992.

5. 5) Er-El, J. and Seginer, A.: Vortex Trajectories and Breakdown on Wing-Canard Configurations, J. Aircraft, 22 (1983), pp. 641–648.

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