Flight dynamics and development of the stability control method of the aero-train (1st report, flight test by pushing)

Yasuaki Kohama; Hideo Watanabe; Satoshi Kikuchi; Fukuo Ohta; Takayuki Itoh

doi:10.1299/kikaib.68.102

Flight dynamics and development of the stability control method of the aero-train (1st report, flight test by pushing)

Yasuaki Kohama, Hideo Watanabe, Satoshi Kikuchi, Fukuo Ohta, Takayuki Itoh

Research output: Contribution to journal › Article

7 Citations (Scopus)

Abstract

Taking into account of the serious greenhouse effect of the Earth, drastic proposal which presents the Carbon Dioxide emission from transportation system must be done. In Japan, over 20% of the Carbon Dioxide is emitted from transportation system. Aero-Train is the new zero-emission high speed vehicle which we are proposing. Wing in ground effect is introduced to obtain highest lift to drag ratio and highest payload. Because of its high efficiency, Aero-Train can be run using only natural energy existing in the space where the vehicle runs. First phase of the present investigation has been done using a running model pushed by a car in the guideway located at the Miyazaki Research Center of RTRI. Results showed that the model successfully floated over 70 km/h around 30 seconds. Best lift to drag ration was 20. Present concept seems to be quite plausible for next generation zero-emission high speed vehicle.

Original language	English
Pages (from-to)	102-107
Number of pages	6
Journal	Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Volume	68
Issue number	665
DOIs	https://doi.org/10.1299/kikaib.68.102
Publication status	Published - 2002 Jan

Keywords

Blade
Greenhouse effect
High speed ground vehicle
Maneuverability
Modeling
Motion control
Natural energy
Propulsion
Wing-in-ground effect
Zero-emission

ASJC Scopus subject areas

Condensed Matter Physics
Mechanical Engineering

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Kohama, Y., Watanabe, H., Kikuchi, S., Ohta, F., & Itoh, T. (2002). Flight dynamics and development of the stability control method of the aero-train (1st report, flight test by pushing). Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 68(665), 102-107. https://doi.org/10.1299/kikaib.68.102

Flight dynamics and development of the stability control method of the aero-train (1st report, flight test by pushing). / Kohama, Yasuaki; Watanabe, Hideo; Kikuchi, Satoshi; Ohta, Fukuo; Itoh, Takayuki.

In: Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, Vol. 68, No. 665, 01.2002, p. 102-107.

Research output: Contribution to journal › Article

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