Development of a Stability Control Method for the Aero-Train-Reference-Cited by-同舟云学术

Development of a Stability Control Method for the Aero-Train

Published:2007 Issue:1 Volume:2 Page:226-237
ISSN:1880-5558
Container-title:Journal of Fluid Science and Technology
language:en
Short-container-title:JFST

Author:

KIKUCHI Satoshi¹,OHTA Fukuo²,KATO Takuma²,ISHIKAWA Tomomi³,KOHAMA Yasuaki²

Affiliation:

1. Gifu University

2. Institute of Fluid Science, Tohoku University

3. AISIN AW Co., Ltd.

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://www.jstage.jst.go.jp/article/jfst/2/1/2_1_226/_pdf

Reference12 articles.

1. (1) Ollia, R. G., Histrical Reverw of WIG Vehicles, J. Hydronautis, 14-3, (1980), pp. 65-76.

2. (2) Ippisch, A. M., Der 'Aerodynamische Bodeneffekt' und die Entwicklung des Flugflchen-(Aerofoil)-Bootes, Luftfahrttechnik Raumfahrttechnik, 10∼, (1964), Nr.10, Oktober, pp. 261-269.

3. Aerodynamic and hydrodynamic aspects of high-speed water surface craft

4. (4) Jorg, G. W., History and Development of the 'Aerodynamic Ground Effect Craft'(AGEC) with Tandem Wings, Symp. Proc. Ram Wing and Ground-Effect Craft, Royal Aeronautical Society, (1987), pp. 87-109.

5. (5) Tomaru, H. and Kohama, Y., Wind-Tunnel Investigation of Aerofoil for Wing in Ground Effect, Journal of Japan Society of Fluid Mechanics, (in Japanese), Vol. 10, (1991), pp. 47-60.

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