• Title/Summary/Keyword: 차세대 초고속 운송시스템

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An Experimental Test for Air-tightness Performance Evaluation of Cracked Concrete Vacuum Tube Structures (콘크리트 진공튜브의 균열 발생에 따른 기밀성능 평가 실험)

  • Park, Joonam;Park, Hyeong-Jun
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.38 no.3
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    • pp.377-385
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    • 2018
  • Super-speed vacuum tube system, where the air resistance is minimized to obtain high speed of the vehicle, is considered to be a viable alternative transportation system. Air-tightness is one of the most important design requirements of the system, because the internal pressure of the system needs to be maintained significantly lower than the atmospheric pressure. This study performed an experimental test, where a series of concrete tube specimens were applied by external loads to induce cracks and the effective air-permeability of the cracked tube structures were measured. The test results indicates that the information on the length and the width of the load-induced cracks are not enough to anticipate the system air-tightness, whereas the load-induced displacement has higher correlation with the systems air-tightness. Based on these results, a direction of future research for effect of the load-induced cracks on the system air-tightness is suggested.

Steady Aerodynamic Characteristics of FAST Flying over Nonplanar Ground Surface (비평면 지면을 비행하는 FAST의 정상상태 공력특성)

  • Cho, Yeon-Woo;Cho, Jeong-Hyun;Cho, Jin-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.6
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    • pp.483-488
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    • 2007
  • The aerodynamic characteristics of FAST(Future Air Speed Transit) combined the body with tandem wing flying over nonplanar ground surface are investigated by using a boundary element method. To validate the present method, results of the present analysis are compared with the experiment and other numerical results. The arrangement of the tandem wing is determined to secure sufficient aero-levitation force and the stability through the analysis of the aerodynamic characteristics of the FAST. The FAST has the maximum lift characteristics when the tandem wing with lower endplate is located at the front side and the rear side of the body. The stability of the FAST can be secured by using the flaperon of the tandem wing.