• Title/Summary/Keyword: RUNWAY

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A Study Shear Behavior of Reinforced Concrete Beams Mixed Steel Fiber (강섬유(鋼纖維)를 혼입(混入)한 철근(鐵筋)콘크리트 보의 전단학동(剪斷學動)에 관(關)한 연구(硏究))

  • Kwak, Kae Hwan;Lee, Kwang Myong
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.11 no.4
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    • pp.1-8
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    • 1991
  • Recently the use of steel fibers has been increased in flexural members and columns of concrete structures subjected to cyclic loadings; such as bridge decks, highway roads, runway of airport, buildings, etc.. However only a few experimental tests have been carried out under fatigue loading. In the present study, the reinforced concrete beams with 1% and 2% steel fiber volume fraction are investigated with and without stirrups. It has been found that in fatigue tests, the failure of the beam is usually due to breaking of fibers rather than fiber pull-out. A comparison of experiments and numerical analysis using the nonlinear F.E.M. program (ADINA) is also presented herein.

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A Case Study on Application of Obstacle Limitation Criteria for Specific Conditions of Airports (특정 조건의 비행장에서 장애물제한규정 적용 사례연구)

  • Kim, DoHyun;Kim, Woong Yi
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.24 no.2
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    • pp.25-30
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    • 2016
  • Obstacle defines all fixed and mobile objects, or parts thereof, that are located on an area intended for the surface movement of aircraft or extend above a defined surface intended to protect aircraft in flight or stand outside those defined surfaces and that have been assessed as being a hazard to air navigation. The airspace around airports are maintained free from obstacles so as to permit the intended aeroplane operations at the airports to be conducted safely and to prevent the airports from becoming unusable by the growth of obstacles around the airports. This is achieved by establishing a series of obstacle limitation surfaces or airspace imaginary surfaces that define the limits to which objects may project into the airspace. This is a case study that shows an application of obstacle limitation criteria, which must be maintained free from an critical obstacle, for specific conditions of two airports. For the purpose of the application, aeronautical studies/flight safety influence assessments were used to identify possible solutions and select a solution that is acceptable without degrading aviation safety.

A Study on a Installation Siting for GBAS Category-I Ground System Implementation in Gimpo Airport (GBAS Cat-I 지상시스템 시범공항 구축을 위한 설치후보지 검토)

  • Bae, Joong-Won;Jeong, Myeong-Sook;Choi, Chul Hee;Ko, Wan-Jin;Ko, Youri;Jun, Hyang-Sig
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.20 no.4
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    • pp.21-30
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    • 2012
  • This paper presents site survey processes and the results for installing GBAS Category-I ground system into Gimpo international airport. For siting assessment, many things should be taken into account in advance, such as installation requirement of GBAS components, future airport development plan and possible interference effects to existing facilities. Because overall performance of GBAS system can be affected by GPS signal reception environment, on-site survey should be performed carefully to measure actual GPS environmental performance and determine if any adverse multipath or RFI problems exist or not. In addtion, VDB antenna should be located to ensure line of sight for transmitting VHF signal to deliver GBAS message to aircraft. Based on the survey results, final location for GBAS system installation is selected near runway 32 in the Gimpo airport.

Commentary Study on Automatic Speedbrake Control System of B747-8 (B747-8 Automatic Speedbrake Control System에 대한 해석적 연구)

  • Moon, Bong Sup;Nam, MyongKwan;Choi, Youn Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.3
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    • pp.40-47
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    • 2018
  • Reducing aircraft speed is the important task in the Rejected Takeoff and/or landing process. It is known that the effect of the Speedbrake is most important factor during the rejected takeoff maneuver in particular near V1 on the critical field length runway. The B747 designer created Automatic Speedbrake Control System to relieve pilot workload, improves brake operation and ensures proper Speedbrake operation for rejected take off. However, those who make the Rejected Takeoff procedure ignored the Automatic function and made it does all manual operations. This lets procedures difficult, complicated, and a cause of confusion and pilot error. This study was conducted to commentary the mechanism and function of the Automatic Speedbrake Control System of B747-8 and to propose appropriate B747-8 Rejected Take off procedures for its function to reduce the workload of pilots and contribute to reduce the possibility of pilot error during Rejected Takeoff.

Comparison with Load Transfer Efficiency for Joint Types in Airport Concrete Pavements (줄눈형식에 따른 공항 콘크리트 포장 하중전달율 비교)

  • An, Ji-Hwan;Jeon, Sung-Il;Kwon, Soo-Ahn;Kim, Min-Woo
    • International Journal of Highway Engineering
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    • v.16 no.3
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    • pp.9-20
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    • 2014
  • PURPOSES : This study is to compare load transfer efficiency of key joint and dowel joint for airport concrete pavement. METHODS : As AC150/5320-6D of FAA's [Advisory Circular] was changed into AC150/5320-6E, Key joint type of rigid pavement were excluded from Construction Joints. LTE(Load Transfer Efficiency) of dowel joint and key joint were compared by times and seasons through pavement temperature measurement, ocular investigation and HWD measurement. RESULTS : For the joint performance grade of No. 2(The second) runway of airport, 12% of poor rate was observed in key joint and 2% of poor rate in dowel joint. Poor rate of key joint was increased to 17%, if only No. 3~No. 6 slabs, which are mostly loaded from the airplanes, were applied for the study. In apron area, LTE poor rate of key joint was high in winter, and LTE poor rate of dowel joint was at least above 'Fair' grade. In summer, 'Fair' for key joint, 'Acceptable' for dowel joint appeared. CONCLUSIONS : As results, dowel joint was superior than key joint for LTE. Deviations of seasons and times were smaller in dowel joint's result. And LTE in winter was lower than LTE in summer.

Guidance and Control System Design for Automatic Carrier Landing of a UAV (무인 항공기의 함상 자동 착륙을 위한 유도제어 시스템 설계)

  • Koo, Soyeon;Lee, Dongwoo;Kim, Kijoon;Ra, Chung-Gil;Kim, Seungkeun;Suk, Jinyoung
    • Journal of Institute of Control, Robotics and Systems
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    • v.20 no.11
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    • pp.1085-1091
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    • 2014
  • This paper presents the guidance and control design for automatic carrier landing of a UAV (Unmanned Aerial Vehicle). Differently from automatic landing on a runway on the ground, the motion of a carrier deck is not fixed and affected by external factors such as ship movement and sea state. For this reason, robust guidance/control law is required for safe shipboard landing by taking the relative geometry between the UAV and the carrier deck into account. In this work, linear quadratic optimal controller and longitudinal/lateral trajectory tracking guidance algorithm are developed based on a linear UAV model. The feasibility of the proposed control scheme and guidance law for the carrier landing are verified via numerical simulations using X-Plane and Matlab/simulink.

Design of Guidance and Control Algorithm for Autolanding In Windshear Environment Using Fuzzy Gain Scheduling (퍼지 게인스케듈링을 적용한 자동착륙 유도제어 알고리즘 설계 : 윈쉬어 환경에서의 착륙)

  • Ha, Cheol-Keun;Ahn, Sang-Woon
    • Journal of Institute of Control, Robotics and Systems
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    • v.14 no.1
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    • pp.95-103
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    • 2008
  • This paper deals with the problem of autolanding for aircraft under windshear environment for which the landing trajectory is given. It is well known that the landing maneuver in windshear turbulence is very dangerous and hard for the pilot to control because windshear is unpredictable in when and where it happens and its aerodynamic characteristics are complicated. In order to accomplish satisfactory autolanding maneuver in this environment, we propose a gain-scheduled controller. The proposed controller consists of three parts: PID controller, called baseline controller, which is designed to satisfy requirements of stability and performance without considering windshear, gain scheduler based on fuzzy logic, and safety decision logic, which decides if the current autolanding maneuver needs to be aborted or not. The controller is applied to a 6-DOF simulation model of the associated airplane in order to illustrate the effectiveness of the proposed control algorithm. It is noted that a cross wind in the lateral direction is included to the simulation model. From the simulation results it is observed that the proposed gain scheduled controller shows superior performance than the case of controller without gain scheduling even in severe downburst and tailwind region of windshear. In addition, touchdown along centerline of the runway is more precise for the proposed controller than for the controller without gain scheduling in the cross wind and the tailwind.

The Influence of Luminous Source on Fabric Chromatic Change Effects (광원색이 직물의 색 변화에 미치는 영향)

  • Jeong, Ji-Yeun;Lee, Eun-Kyung
    • Journal of the Korean Home Economics Association
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    • v.48 no.5
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    • pp.17-24
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    • 2010
  • Although design, color, and material are important elements in stage costumes, stage lightning also plays significant role in the presentation of stage costumes. Costumes color, material and perception can be significantly influenced by visual effects. Stage illumination can be arranged or managed so that colors are closely related to or enhanced or change the effects of costume colors on the runway or display at specific times. The results of this thesis are as follow; 1) Fabric tone, name, brightness, and chroma of colors were changed by the colors of stage lighting. 2) An achromatic color was changed to a chromatic color after being combined with colors of stage lighting. 3) Stage illuminations can make fabric, colors look similar to stage colors. 4) Plain satin silk fabric which reflects light shows high brightness and chroma after being influenced by stage lighting its shining effects and color changes were clear and apparent. 5) Velvet pile fabric which absorbs light shows low brightness and chroma after being influenced by stage lightning its shining effects and changes of colors were not clear and apparent. In conclusion, natural lights did not significantly influence fabric colors and perception, while artificial lights had wide range of effects on fabric colors and perception.

A Case Study of Art Marketing in Fashion Brand

  • Hong, Sung-Sun;Hwang, Choon-Sup
    • Journal of Distribution Science
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    • v.11 no.11
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    • pp.19-32
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    • 2013
  • Purpose - This study examines the effects of art marketing management of the marketing mix in fashion, focusing on the cases of the leading global fashion brands in art marketing management. Research Design, Data, and Methodology - This study was implemented using the content analysis method. Criteria, including product differentiation, promotion strategies, store strategies, and social contributions, were based on previous research, brand promotional references, and critical reviews in newspapers or professional magazines for various cases of art marketing management by fashion brands. Results - To achieve product differentiation, art marketing management has borrowed images from artworks, and employed parodies and collaboration with artists; this has facilitated the pleasure derived from utilizing the artistic value of products. Promotion strategies were integrated with art performances, advertisements, and runway shows. Store strategies developed emotional feelings and a longing for brands among consumers. Reputational marketing of the social contributions made by corporations elevated the corporate brand image perceived by consumers. Conclusions - This study's findings revealed that consumers can derive emotional satisfaction through art marketing that seeks to profit effectively by stimulating consumers' emotions. From an economic perspective, a convergence of art and marketing plays an important role in profit-making and satisfying consumers' emotions.

A Study on the Antiabrasion of the Aircraft Carbon Disk Brake (항공기의 탄소 디스크 브레이크의 내마모성에 관한 연구)

  • Lee, Jang-Hyun;Yum, Hyun-Ho;Hong, Min-Sung
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.6
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    • pp.968-975
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    • 2012
  • ABS(Anti-skid Brake System) had been developed on purpose of most effect at breaking in limited runway. An aircraft has a large amount of kinetic energy on landing. When the brakes are applied, the kinetic energy of the aircraft is dissipated as heat energy in the brake disks between the tire and the ground. The optimum value of the slip during braking is the value at the maximum coefficient of friction. An anti-skid system should maintain the brake torque at a level corresponding to this optimum value of slip. This system is electric control system for brake control valve at effective control to prevent slip and wheel speed or speed ratio. In this study we measured the thickness of the carbon disk before and after to find its wear and it shows that carbon disk brake has higher stiffness and strength than metal disk at high temperature. In addition, thermal structural stability and appropriate frictional coefficient of the carbon disk brake prove its possible substitution of metal disk brake.