1 |
Johnson, B. Jr., and Demele, F. D., 'Investigation of a Thin Wing of Aspect Ratio 4 in The Ames 12-Foot Pressure Wind Tunnel. III The Effectiveness of Constant-Chord Aileron', NACA RM-A8I17, 1948
|
2 |
한철희, 조진수, '지면근처를 비행하는 날개의 WIG효과에 대한 정상상태 공력해석', 한국항공우주학회지, 제28권 제3호, 2000, pp. 46-52
|
3 |
Han, C., Cho, J., Moon, Y, Yoon, Y., and Song, Y, 'Design of an Aero-levitation Electric Vehicle for High-Speed Ground Transportation System', Journal of Aircraft, Vol. 42, No.1, 2005, pp. 93-104
DOI
ScienceOn
|
4 |
철도건설규칙 (건설교통부령 제453호) 제4장 전철전력 제44조 1항, 2005년 7윌 6일
|
5 |
Han, C., 'Aerodynamic Analysis and Design of an Aero-levitation Vehicle for a High speed Ground Transportation System', Ph.D. Dissertation, Department of Mechanical Engineering, Hanyang University, 2003
|
6 |
Mithra, S., 'The Tracked Wing in Ground -Effect(TWIG)', Ph.D. Thesis, Faculty of Mechanical and Aerospace Engineering, Princeton University, UMI, Michigan, 1983
|
7 |
Kono, T., Kohama, Y., and Matsui, N., 'Stability Guide Way Type Wing in Ground Effect Vehicle', Proceeding of the Third JSME-KSME Fluids Engineering Conference, JSME, Sendai, Japan, 1994, pp. 715-718
|
8 |
William, H. A, and William, R. E., 'Configuration Effect on the Lift of a Body in Close Ground Proximity', Journal of Aircraft, Vol. 13, No.8, 1976, pp. 584-589
DOI
ScienceOn
|
9 |
Katz, J., and Plotkin, A., Low-Speed Aerodynamics, 2nd Ed., Cambridge University Press, New York, 2001
|