Design of an aero-levitation electric vehicle for the high-speed ground transportation system

Jinsoo Cho; Cheolheui Han; Young June Moon; Younghyun Yoon; Yongkyu Song

Design of an aero-levitation electric vehicle for the high-speed ground transportation system

Jinsoo Cho, Cheolheui Han, Young June Moon, Younghyun Yoon, Yongkyu Song

Department of Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

2 Citations (Scopus)

Abstract

An Aero-levitation Electric Vehicle (AEV) as a Tracked Wing-In-Ground-effect vehicle (TWIG) is proposed as a promising form of next generation transport. The development of the High-speed Ground Transportation System (HGTS) requires the careful consideration of the aerodynamic interaction of the AEV with the Guideway. It is investigated through the following multidisciplinary cooperation: aerodynamic analysis using the potential flow theory and the Navier- Stokes computation, wind-tunnel measurements using the scaled model system, and dynamic simulations for the given flight missions. The recent results from these multidisciplinary studies will be summarized and addressed.

Original language	English
Title of host publication	AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum
Publication status	Published - 2002 Dec 1
Event	AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum - Los Angeles, CA, United States Duration: 2002 Oct 1 → 2002 Oct 3

Other

Other	AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum
Country	United States
City	Los Angeles, CA
Period	02/10/1 → 02/10/3

ASJC Scopus subject areas

Aerospace Engineering
Mechanical Engineering

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Cite this

Cho, J., Han, C., Moon, Y. J., Yoon, Y., & Song, Y. (2002). Design of an aero-levitation electric vehicle for the high-speed ground transportation system. In AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum

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abstract = "An Aero-levitation Electric Vehicle (AEV) as a Tracked Wing-In-Ground-effect vehicle (TWIG) is proposed as a promising form of next generation transport. The development of the High-speed Ground Transportation System (HGTS) requires the careful consideration of the aerodynamic interaction of the AEV with the Guideway. It is investigated through the following multidisciplinary cooperation: aerodynamic analysis using the potential flow theory and the Navier- Stokes computation, wind-tunnel measurements using the scaled model system, and dynamic simulations for the given flight missions. The recent results from these multidisciplinary studies will be summarized and addressed.",

author = "Jinsoo Cho and Cheolheui Han and Moon, {Young June} and Younghyun Yoon and Yongkyu Song",

year = "2002",

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language = "English",

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T1 - Design of an aero-levitation electric vehicle for the high-speed ground transportation system

AU - Cho, Jinsoo

AU - Han, Cheolheui

AU - Moon, Young June

AU - Yoon, Younghyun

AU - Song, Yongkyu

PY - 2002/12/1

Y1 - 2002/12/1

N2 - An Aero-levitation Electric Vehicle (AEV) as a Tracked Wing-In-Ground-effect vehicle (TWIG) is proposed as a promising form of next generation transport. The development of the High-speed Ground Transportation System (HGTS) requires the careful consideration of the aerodynamic interaction of the AEV with the Guideway. It is investigated through the following multidisciplinary cooperation: aerodynamic analysis using the potential flow theory and the Navier- Stokes computation, wind-tunnel measurements using the scaled model system, and dynamic simulations for the given flight missions. The recent results from these multidisciplinary studies will be summarized and addressed.

AB - An Aero-levitation Electric Vehicle (AEV) as a Tracked Wing-In-Ground-effect vehicle (TWIG) is proposed as a promising form of next generation transport. The development of the High-speed Ground Transportation System (HGTS) requires the careful consideration of the aerodynamic interaction of the AEV with the Guideway. It is investigated through the following multidisciplinary cooperation: aerodynamic analysis using the potential flow theory and the Navier- Stokes computation, wind-tunnel measurements using the scaled model system, and dynamic simulations for the given flight missions. The recent results from these multidisciplinary studies will be summarized and addressed.

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M3 - Conference contribution

SN - 9781624101250

BT - AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum

T2 - AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum

Y2 - 1 October 2002 through 3 October 2002

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