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

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

Volumn , Issue , 2002, Pages

  Cho, Jinsoo ^a   Han, Cheolheui ^a   Moon, Youngjune ^b   Yoon, Younghyun ^c   Song, Yongkyu ^d  

^a Hanyang University   (South Korea)

^b Korea University   (South Korea)

^c Korean Air Force Academy   (South Korea)

^d Hankuk Aviation University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATION THEORY; ELECTRIC AUTOMOBILES; FLIGHT SIMULATORS; GROUND EFFECT; NAVIER STOKES EQUATIONS; WIND TUNNELS;

AERO-LEVITATION ELECTRIC VEHICLE; AERODYNAMIC ANALYSIS; AERODYNAMIC INTERACTIONS; GROUND TRANSPORTATION SYSTEMS; NAVIER-STOKES COMPUTATIONS; POTENTIAL-FLOW THEORY; WIND TUNNEL MEASUREMENTS; WING-IN-GROUND EFFECT VEHICLES;

AIR CUSHION VEHICLES;

EID: 85085773763     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-5829     Document Type: Conference Paper

References (6)

1. Kono, T. et al, "Stability of Guide Way Type Wing in Ground Effect Vehicle," Proceedings of the third JSME-KSME Fluids Engineering Conference, June 1994, pp. 715-718
2. Kohama, Y. P., Kikichi, S. Watanabe, H., Ohta, F. and Ito, T., "Evaluation of the Transportation System in relation to Environmental Problem," Workshop on Drag Reduction of Aircraft and Ground Transportation, Institute of Fluid Science, Tohoku University, Sendai, Japan, August 18, 2000
3. Jinsoo C., Cheolheui, H., Youngjune, M. and Jaehyun, B., "Aerodynamic Analysis and Design of an Aero-levitation Electric Vehicle," AIAA-CP-2435, 2001
4. Sankrithi, M., "The Tracked Wing In Ground- Effect," Ph. D. Dissertation, Department of Mechanical and Aerospace Engineering, Princeton University, 1983
5. Kikuchi, K., "Numerical Simulation of the Ground Effect using the Boundary Element Method," International Journal for Numerical Methods in FLUIDS, Vol. 25, 1997, pp.1043-1056
6. Hall, I., "An investigation into the flight dynamics of Wing In Ground effect aircraft operating in aerodynamic flight," Cranfield College of Aeronautics, september, 1994.