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      외부장착물지지 주익구조 정적 시험 및 해석 = Static Test and Analysis of Wing Support Structure for External Stores

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      https://www.riss.kr/link?id=A101834987

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      다국어 초록 (Multilingual Abstract)

      Armed aircraft of a basic trainer class installs external stores under wing box by using pylon and performs an operation such as weapon delivery and jettison, and should be designed to withstand all kinds of loads applied to external stores. The static strength test of pylons and wing box was performed to assess the static strength of pylon and their support structures for substantiation. Based on the test, the structures were verified to fully satisfy a given design requirement. In this paper, methods of test load generation of wing box and pylon, evaluation of test result data and design result of test set-up were presented. Comparing the FEM analysis with the same test data can lead to good match and reasonable deviation between both. Finally, based on the test and the analysis, the static strength of test article was substantiated and the reliability and effectiveness of analysis math model were obtained.
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      Armed aircraft of a basic trainer class installs external stores under wing box by using pylon and performs an operation such as weapon delivery and jettison, and should be designed to withstand all kinds of loads applied to external stores. The stati...

      Armed aircraft of a basic trainer class installs external stores under wing box by using pylon and performs an operation such as weapon delivery and jettison, and should be designed to withstand all kinds of loads applied to external stores. The static strength test of pylons and wing box was performed to assess the static strength of pylon and their support structures for substantiation. Based on the test, the structures were verified to fully satisfy a given design requirement. In this paper, methods of test load generation of wing box and pylon, evaluation of test result data and design result of test set-up were presented. Comparing the FEM analysis with the same test data can lead to good match and reasonable deviation between both. Finally, based on the test and the analysis, the static strength of test article was substantiated and the reliability and effectiveness of analysis math model were obtained.

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      참고문헌 (Reference)

      1 이영오, "XKT-1항공기 파일런 정적구조시험 및 해석 연구" 2007

      2 Federal Aviation Regulation, "Part23Airworthiness Standards : Normal, Utility, and Aerobatic Category Airplanes"

      3 "Metallic Material Properties Development and Standardization(MMPDS)"

      4 "Airplane Strength and Rigidity, Ground Tests"

      5 "Airborne stores, suspension equipment and aircraft-store interface(carriage phase)"

      6 "AIRCRAFT STORES/SUSPENSION EQUIPMENT STRUCTURAL INTEGRITY GROUND TEST"

      1 이영오, "XKT-1항공기 파일런 정적구조시험 및 해석 연구" 2007

      2 Federal Aviation Regulation, "Part23Airworthiness Standards : Normal, Utility, and Aerobatic Category Airplanes"

      3 "Metallic Material Properties Development and Standardization(MMPDS)"

      4 "Airplane Strength and Rigidity, Ground Tests"

      5 "Airborne stores, suspension equipment and aircraft-store interface(carriage phase)"

      6 "AIRCRAFT STORES/SUSPENSION EQUIPMENT STRUCTURAL INTEGRITY GROUND TEST"

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2026 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2017-01-01 평가 등재학술지 선정 (계속평가) KCI등재
      2015-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.29 0.29 0.29
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.28 0.26 0.323 0.31
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