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Static Test and Analysis of Wing Support Structure for External Stores

외부장착물지지 주익구조 정적 시험 및 해석

  • Received : 2015.01.22
  • Accepted : 2015.02.13
  • Published : 2015.03.31

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.

Keywords

References

  1. MIL-A-8591H, "Airborne stores, suspension equipment and aircraft-store interface(carriage phase); General Design Criteria for
  2. MIL-A-008867B, "Airplane Strength and Rigidity, Ground Tests"
  3. MIL-HDBK-1763, "AIRCRAFT STORES/ SUSPENSION EQUIPMENT STRUCTURAL INTEGRITY GROUND TEST"
  4. Federal Aviation Regulation(FAR), Vol.III, Part23 Airworthiness Standards : Normal, Utility, and Aerobatic Category Airplanes
  5. MMPDS-8, "Metallic Material Properties Development and Standardization(MMPDS)
  6. 이영오, 장재호, 김성휘, 김형석, 조대현, "XKT-1 항공기 파일런 정적구조시험 및 해석 연구" KSAS07-3170, 한국항공우주학회 추계학술대회 2007