• Title/Summary/Keyword: Kim test

Search Result 52,951, Processing Time 0.071 seconds

A Study on the Design and Verification-Validation of the Supportive Equipment for Shipyard Test of Naval Combat System (함정 전투체계 함상시험을 위한 지원장비 설계 및 검증 연구)

  • Jung, Youngran;Kim, Cheolho;Han, Woonggie;Kim, Jaeick;Kim, Hyunsil
    • Journal of the Korea Institute of Military Science and Technology
    • /
    • v.17 no.3
    • /
    • pp.318-326
    • /
    • 2014
  • The Shipyard Test of Naval Combat System depends on external factors, such as weather conditions and availability of its sensor-weapon, due to the need of on-board sensor-weapon during the test. This paper suggests the Supportive Equipment using virtual simulator for Shipward Test, in case of the unavailability of the on-board sensor-weapon or the test support force(aircraft, surface ship etc.), to pre-check the functions of the combat system as well as to prepare the Shipyard Test. To mock the real sensor-weapon functions as similar as possible, the Supportive Equipment for Shipyard Test was verified by the Verification and Validation process, which is usually performed while developing models in the Modeling & Simulation field.

A Study of Enhanced Test Maturity Model with Test Process Improvement (테스트 프로세스 개선모델을 통한 테스트 성숙도 모델 (Test Maturity Model) 확장에 관한 연구)

  • Kim, Ki-Du;Kim, Young-Chul
    • The KIPS Transactions:PartD
    • /
    • v.14D no.1 s.111
    • /
    • pp.57-66
    • /
    • 2007
  • Organizations of Software development are very important issue on enhancement of a software quality as rapid progress of software industry. Especially there are diverse attempts for enhancement of test maturity of the software organization through some kinds of the test maturity model. But the current test maturity models based on CMM(Capability Maturity Model) lack part of actual testing measurement and only measure level of test maturity. To solve these problems, we suggest 'double V-model' to execute both software development process and test process simultaneously, and also 'test attributes to Maturity Levels Correlation Matrix' for evaluating level of test maturity included with definitions of test attribute and level. That is, we enhance TMM(Test Maturity Model) adopted with 'Improvement Suggestion' of TPI(Test Process Improvement) which is easy the evaluation of test maturity of organization and gives the direction of improvement to level up the test maturity for the measured organization. As a result, we will contribute to level up the test maturity of the organization.

Guideline for Test Process Improvement of Test Organization Through Correlating TMMi with TPI NEXT (상관관계를 통한 조직의 테스트 프로세스 개선 가이드 방안)

  • Kim, Kidu;Park, Young Bom;Kim, R. Youngchul
    • KIPS Transactions on Software and Data Engineering
    • /
    • v.2 no.12
    • /
    • pp.823-828
    • /
    • 2013
  • In this paper, it will improve in quality to adapt a right test process which is formalized from certification of TMMi Level. To do this, we suggest correlative relation through analyzing associations between TMMi and TPI next based on the previous research[10], which provides the guideline for enhancing test process level with measuring Test maturity model. Also schematize test maturity measurement through refining and improving the previous test maturity correlation metrics[6,8,9]. As one example with limited level, it shows the guideline to improve test process of one testing organization through improved correlation metrics with TMMi and TPI next.

Development of Turbopump Cavitation Performance Test Facility and the Test of Inducer Performance (터보펌프 Cavitation 성능시험기 개발 및 성능시험에 관한 연구)

  • Sohn, Dong-Kee;Kim, Chun-Tak;Yoon, Min-Soo;Cha, Bong-Jun;Kim, Jin-Han;Yang, Soo-Seok
    • Proceedings of the KSME Conference
    • /
    • 2001.06e
    • /
    • pp.619-624
    • /
    • 2001
  • A performance test facility for turbopump inducer cavitation was developed and the inducer cavitation performance tests were performed. Major components of the performance test facility are driving unit, test section, piping, water tank, and data acquisition and control system. The maximum of testing capability of this facility are as follows: flow rate - 30kg/s; pressure - 13 bar; rotational speed 10,000rpm. This cavitation test facility is characterized by the booster pump installed at the outlet of the pump that extends the flow rate range, and by the pressure control system that makes the line pressure down to vapor pressure. The vacuum pump is used for removing the dissolved air in the water as well as the line pressure. Performance tests were carried out and preliminary data of test model inducer were obtained. The cavitation performance test and cavitation bubble flow visualization were also made. This facility is originally designed for turbopump inducer performance test and cavitation test. However it can be applied to the pump impeller performance test in the future with little modification.

  • PDF

The Vibration Characteristic and Fatigue Life Estimation of a Small-scaled Hingeless Hub System with Composite Rectangular Blades (복합재료 기준형 블레이드를 장착한 축소 힌지없는 허브시스템의 진동특성과 피로수명 예측)

  • Song, Keun-Woong;Kim, Jun-Ho;Kim, Duck-Kwan;Joo, Jin
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
    • /
    • 2003.11a
    • /
    • pp.310-315
    • /
    • 2003
  • This paper described that rotating test and fatigue test of a small-scale hingeless hub system with composite rectangular blades. Generally Rotating stability and fatigue test technique is one of Key-technology on test and evaluation for helicopter rotor system Rotating test of hingeless rotor system was achieved by means of rotor vibration characteristic and aeroelastic stability test GSRTS, equipped with hydraulic actuator and 6-component rotating balance was used to test hingeless rotor system especially for an observation of blade motion including flawing, lagging and feathering. Rotating test was done in hover and forward flight condition. Small-scaled blade fatigue test condition was determined by blade load analysis with the reference table of composite materials(S-N curve). Fatigue test bench was developed for the estimation of blade fatigue life, and tested its characteristic.

  • PDF

Flight Test Method to Show Compliance to Fuel System Airworthiness Requirements of Small Aircraf (소형 비행기 연료 계통 적합성 입증을 위한 비행시험에 관한 고찰)

  • Kim, Seungkyem
    • Journal of Aerospace System Engineering
    • /
    • v.6 no.3
    • /
    • pp.34-39
    • /
    • 2012
  • In this paper, analysis of airworthiness requirements which require flight test to show compliance and flight test method as means of compliance to those requirements are provided. For unusable fuel test, sufficient discussion between certification authority and applicant is required to select test conditions. For hot weather fuel system operation test, preservation and heating of test fuel should be done carefully not to adversely affect to test result.

New Test for IDMRL(DIMRL) Alternatives using Censored Data

  • Na, Myung-Hwan;Lee, Hyun-Woo
    • Journal of the Korean Data and Information Science Society
    • /
    • v.10 no.1
    • /
    • pp.57-65
    • /
    • 1999
  • In a resent paper, Na, Lee and Kim(1998) develop a test statistic for testing whether or not the mean residual life changes its trend based on complete data and show that the new test performs better than previously known tests. In this paper, we extend their test to the randomly censored data. The asymptotic normality of the test statistic is established. Monte Carlo simulations are conducted to compare our test with a previously known test by the power of tests.

  • PDF