• 상하수도학회지
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• 제22권6호
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• pp.681-687
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• 2008

It is well known that the water infiltration rate depends on soil properties such as soil water content, water head, capillary suction, density, hydraulic conductivity, and porosity. However, most of proposed infiltration models assume that the air phase is continuous and in equilibrium with the atmosphere or air compression and air entrapment on infiltration was not considered. This study presents experimental results on unsaturated water infiltration to relate air entrapment and hydraulic conductivity function based on soil air properties. The objectives of this study were to measure change of soil air pressure ahead of wetting front under air drain and air confined condition to find the confined air effect on infiltration rate, to reduce the entrapped air volume related with soil air pressure to increase the soil permeability, and to make a basis of infiltration process model for the purpose of improvement of infiltration rate in the homogeneous soil column. The results of the work show that soil air pressure increases according to increasement of the saturated soil depth rather than the wetting front depth during infiltration process.

• 한국항공운항학회지
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• 제12권3호
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• pp.41-63
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• 2004

The area covered by product liability in broadest sense is so vast that an attempt to analyse all its impact on the aviation world risk. Every effort has been made to confine our review of subject a closely as possible to its influence on aircraft manufacturers, airlines and passengers, in spite of strong connections with other spheres of commercial. Product Liability in aviation is the liability of aircraft's manufacturer, processor or non-manufacturing seller for injury to the person or property of a buyer or third party caused by a product which has been sold. Here-in a product is aircraft, third party is passengers who suffered damage by defective design, defective construction, inadequate instructions for handling in aircraft. Whenever a product turns out to be defective after it has been sold, there are under Anglo-American law three remedies available against the aircraft's manufacturer (1) liability for negligence (2) breach of warranty (3) strict liability in tort. There are Under continental law Three remedies available against the aircraft's manufacturer (1) liability for defective warranty (2) liability for non-fulfillment of obligation (3) liability in tort. It is worth pointing out here an action for breach of warranty or for defective warranty, for non-fulfillment of obligation is available only to direct purchaser on the basis of his contract with the aircraft's manufacturer, which of course weakness its range and effectiveness. An action for tort offers the advantage of being available also to third parties who have acquired the defective product at a later stage. In tort, obligations are constituted not only by contract, but also by stature and common law. In conclusion, There in no difference in principle of law. In conclusion I would like to make few suggestions regarding the product liability for aircraft's manufacturer. Firstly, current general product liability code does not specify whether government offices(e.g. FAA) inspector conducted the inspection and auditory certificate can qualify as conclusive legal evidence. These need to be clarified. Secondly, because Korea is gaining potential of becoming aircraft's manufacturer through co-manufacturing and subcontracting-manufacturing with the US and independent production, there needs legislation that can harmonize the protection of both aircraft's manufacturers and their injured parties. Since Korea is in primary stage of aviation industry, considerate policy cannot be overlooked for its protection and promotion. Thirdly, because aircraft manufacturers are risking restitution like air-carriers whose scope of restitution have widened to strict and unlimited liability, there needs importation of mandatory liability insurance and national warranty into the product liability for aircraft's manufacturers. Fourthly, there needs domestic legislation of air transportation law that clearly regulates overall legal relationship in air transportation such as carrier & aircraft manufacturer's liability, and aviation insurance.

• 한국지반공학회논문집
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• 제29권6호
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• pp.53-62
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• 2013

NATM공법을 이용한 터널 시공에서 초기에 원지반을 구속시키고 암반과의 일체화를 통해 터널의 안정성을 확보하기 위해 통상 5-20cm 두께의 숏크리트를 시공하며 여기에는 강섬유가 $40kg/m^3$ 정도 포함되도록 설계하고 있다. 숏크리트 내에 혼합된 강섬유는 숏크리트를 뿜어 내는 장비 특성, 혼합비 그리고 현장 암반 상태에 따라 숏크리트 내 강섬유가 골고루 분산될 수도 있고 그렇지 않을 수도 있다. 본 연구에서는 단면이 $15cm{\times}15cm$이고 길이 55cm인 사각기둥 모양의 시멘트 혼합비가 5% 또는 20%인 공시체를 3cm씩 다섯 층으로 나누어 강섬유를 혼합하지 않거나, 중간층만 혼합하거나, 1, 3, 5층만 혼합하거나, 전층을 혼합한 네 종류의 숏크리트를 모사한 콘크리트 공시체를 제작하였다. 7일 동안 공시체를 대기중 양생한 다음 휨강도시험을 실시하여 층별로 강섬유가 분산되거나 집중될 경우 휨강도와 인성에 미치는 영향에 대하여 연구하였다. 시멘트 혼합비가 20%인 경우 강섬유 혼합층이 증가할수록 휨강도는 증가하였으며, 동일한 양의 강섬유가 골고루 분산되지 않고 한 곳으로 집중될 경우 휨강도가 20% 정도 감소하였다. 한편 시멘트 혼합비가 5%로 낮은 경우에는 강섬유 혼합층이 증가할수록 오히려 휨강도는 감소하였다. 시멘트 혼합비에 관계없이 강섬유 혼합층이 증가할수록 인성지수는 점점 증가하는 경향을 보였으며, 강섬유가 중간층으로 집중된 경우보다 골고루 분산된 경우 인성지수는 2-3배 정도 증가하였다.