• Aerospace Industry
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• v.21
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• pp.21-23
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• 1994

• Defense and Technology
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• no.5 s.63
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• pp.5-11
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• 1984

• Defense and Technology
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• no.3 s.109
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• pp.16-30
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• 1988

• Defense and Technology
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• no.3 s.121
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• pp.12-29
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• 1989

• Defense and Technology
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• no.12 s.202
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• pp.62-67
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• 1995

• Journal of the Korea Institute of Military Science and Technology
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• v.16 no.3
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• pp.277-284
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• 2013

In this paper, the ventilating and heating system of T-103 trainer aircraft were investigated and redesigned to improve its poor performance. The ventilation system of the trainer was designed to increase the mass flow rate of fresh air by using air intake valves. The flow-in air through the air intake valve is supplied to the cabin by the ram effect of aircraft and the propeller. And the additional heating system was installed to improve the temperature of the cabin inside. The wasted heat from the exhaust gas of the engines was used as heat source of the additional heating system by installing an heat exchanger around the exhaust nozzle. The additional fresh air and the heated air enter the cabin via two ducts mounted under the instrument panel and behind the pedal in the cabin. The additional ventilating and heating system can be controlled by the first pilot and the secondary pilot individually using the control knob equipped separately. After mounting the additional ventilating and heating system, evaluations such as inspection of parts and component, ground run-up test, in-flight test, user test, etc. were conducted. The result of the tests was sufficient to meet the requirements of the manuals, and the pilots were satisfied with the additionally mounted systems.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.225-229
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• 2003

The exact performance simulation of propulsion system is a key element in the prediction of the aircraft performance. The specification performance analysis using the installed loss of KT-1 showed a large difference with the engine performance measured during the flight tests. This indicates that a method to estimate the more exact performance is needed. The study on the performance simulation with performance map correction along the engine operating line shows the good consistent results through all the flight conditions and engine conditions. The correction factors of the map were resulted from the comparative analysis between the flight test and the simulation of installed engine performance.

• Defense and Technology
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• no.8 s.174
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• pp.44-51
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• 1993

F-5 성능개량의 근본적인 배경은 경제성입니다. F-16 한대 도입할 가격이면 대략 10대의 F-5 성능개량이 가능하므로 비용 대 효과 측면에서 많은 국가들이 매력을 느끼고 있습니다 또한 선도 훈련기로서의 필요성이 전투기.성능이 급격히 높아짐에 따라, 성능개량되는 F-5 수준의 항공기로 예비훈련을 함으로써, 고성능 전투기의 비전력화 훈련소요를 상당부분 대체할수 있습니다

• Journal of Convergence for Information Technology
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• v.10 no.6
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• pp.217-227
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• 2020

This study investigated the effects of dual task training on balance, upper extremity motor function and activities of daily living in patients with chronic stroke. The study subjects were 14 chronic stroke patients. dual task training groups(n=7), and single task training groups(n=7). The intervention period was conducted for 3 times a week, 30 minutes per session, and 4 weeks for all groups. To measure the BT4, JTT, K-MBI were used before and after the intervention. Dual task training groups showed a significant increase in BT 4 and JTT scores(p<.05). The difference between the two groups was significant in the BT4 and JJT scores(p<.05). There was a score improvement in K-MBI, but there was no statistically significant difference(p>.05) Dual task training was effective in facilitating balance, upper extremity function and activities of daily living in patients with chronic stroke.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.5
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• pp.127-133
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• 2002

The general requirements to achieve the structural integrity of the airframe are described in the military specification, MIL-STD-1530A. One of these requirements is the durability and damage tolerance of the airframe, which should be shown through the analysis and test based on the related specifications. This paper introduces the full scale durability test to evaluate the structural safety and durability of the basic trainer, KT-1. The test was performed according to the procedure in the military specification. The flight by flight load spectrum was developed by KT-1 fatigue load criteria and used for the durability test. The durability test had been performed for 4 service lives and was completed successfully. Therefore, it was shown that KT-1 airframe satisfied the durability requirements.