• Proceedings of the Korean Institute of Building Construction Conference
• /
• 2017.05a
• /
• pp.137-138
• /
• 2017

The Waterproofing and Anti corrosion materials applied to the water supply facility did not consider environment of water supply facility, thus defects occurred consistently on the site. In this study, it suggests safety adhesion test of wet surface and have a test for safety adhesion performance.

• The Journal of the Korea Contents Association
• /
• v.16 no.11
• /
• pp.154-165
• /
• 2016

The purpose of this study is to see the effect of the art therapy in group on the work stresses and emotional burnouts of social workers for diabled facility. The subjects are the 8 members of social workers at the facility for disabled located in city A. From Feb 16, 2016 to May 31, 2016, 70 minutes per session, overall 13 therapies were given. To see the therapeutic effects, there were test of stress and burnout before, afterwards and 4 weeks later. To find out the similarities in group, Mann Whitney U test was done, and Wilcoxon's signed ranks test was done to see the difference afterwards. As a result, art therapy in group was effective on the work stress and burnout of social workers in daisabled facility and the positive effect lasted. This results suggests a developed ways to reduce work stress and emotional burnout of social workers for disabled facility.

• Journal of Korean Ophthalmic Optics Society
• /
• v.9 no.1
• /
• pp.167-171
• /
• 2004

The accommodative facility test can be use the very benetit in visual function test. The purpose of this study was mainly to check the binocular function and to estimate the amount of accommodation with the hand held flipper. It was measured as the subjective time needed to clear an accommodative target (20/20 letters) at 40 em through +/-2.00 D flipper(Bernell Corp., USA). The subjects have an irrespective of sex and no eye disease. Seventy five of youth applicants participated for the accommodative facility test. The reagents using the flipper had higher expected value than the other reagents. In test for the binocular function, the accommodative facility test is a important part due to a serviceable and simple examination. Therefore, these binocular checkup have to be developed through a survey of normative value in the near future.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2001.11a
• /
• pp.282-287
• /
• 2001

The test facility has been manufactured to predict the dynamic insertion loss and the pressure drop for ducted silencers based on ISO 7235. The qualification test of the test facility is necessary for determining the dynamic insertion loss and the pressure drop of the test silencer, and is surveyed the reflection coefficient for an anechoic termination, the velocity profile near the upstream connection to the test silencer, the reduction of the system silencer and the limiting insertion loss due to the flanking sound transmission along the duct walls.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2003.10a
• /
• pp.13-19
• /
• 2003

A supersonic ground test facility to develop Ramjet and SCRamjet(Supersonic Combustion Ramjet) engine should be able to simulate high altitude and high Mach number conditions including air total pressure, oxygen level and specific heat ratio at the combustion chamber entrance. The test facility also should simulate the effect of oblique shock wave caused by the flight vehicle. The test facility developed in this study is supersonic free-jet blowdown type, which consists of high pressure air supply source(maximum pressure=32MPa), air heater(vitiation type), supersonic diffuser, ejector, and test chamber(nozzle exit dimension=200mm$\times$200mm).

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2006.11a
• /
• pp.43-46
• /
• 2006

Storage air heater(SAH) is a general purpose facility that is used to simulate the high altitude condition of supersonic ground test facility, thurst compensation test of rocket engine nozzle and gas turbine engine combustor test. SAH in KARI is built to simulate the total temperature of the supersonic ground test facility which has a wide flight envelope from altitude 0km, Mach 2 to altitude 25km, Mach 5 and operates up to 1300K, 3.5MPa. In this paper, we introduces the SAH in JAXA which is model of SAH in KARI and summarizes the design process and manufacture of ours.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2006.11a
• /
• pp.75-81
• /
• 2006

The propulsion system of KSLV-I second stage is engine with high expansion ratio and its starting altitude is high. To verify the performance of engine before the launch in the ground, high altitude test facility to simulate its operating condition is necessary. This material is about the concept design of high altitude simulation test facility for second stage engine. And it will be the basis for the construction of test facility and the test of engine.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.7 no.4
• /
• pp.53-62
• /
• 2003

A supersonic ground test facility to develop Ramjet and SCRamjet(Supersonic Combustion Ramjet) engine should be able to simulate high altitude and high Mach number conditions including air total pressure, oxygen level and specific heat ratio at the combustion chamber entrance. The test facility also should simulate the effect of oblique shock wave caused by the flight vehicle. The test facility developed in this study is supersonic free-jet blow down type, which consists of high pressure air supply source(maximum pressure=32MPa), air heater(vitiation type), supersonic diffuser, ejector, and test chamber(nozzle exit dimension=200mm${\times}$200mm).

• Journal of the Korean Society of Propulsion Engineers
• /
• v.12 no.1
• /
• pp.37-43
• /
• 2008

In order to verify the performance of upper stage propulsion system designed to operate in the upper atmosphere, test facility which can simulate high altitude is needed. Cylindrical supersonic exhaust diffuser, which utilizes the momentum of exhaust gas, provides a simple means for providing a low pressure around the propulsion system. This paper describes sub-systems and specification of high altitude test facility developed for the test of KSLV-I kick motor. Performance of the facility has been successfully verified through five times of hot firing tests.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.04a
• /
• pp.109-112
• /
• 2011

The result of design review and arrangement of a combustion chamber test facility(CTF) and a turbo-pump real propellant test facility(TPTF) is briefly described. The development/qualification tests of combustion chamber and turbo-pump for 75ton-class liquid rocket engine will be performed in CTF and TPTF. The critical design of hydraulic-pneumatic system, control and data acquisition system, test stand cell, and auxiliary facilities in CTF and TPTF was performed.