Verification test of the structural integrity of an external fuel tank for aircraft under slosh and vibration conditions

Author:

Kim Hyun-gi1ORCID,Kim Sungchan1,An Su-hong2,Ha Byung-geon2

Affiliation:

1. Aeronautics Technology Research Division, Aeronautics Research Directorate, Korea Aerospace Research Institute, Daejeon, Republic of Korea

2. Hanwha Aerospace Co, Asan-si, Republic of Korea

Publisher

Informa UK Limited

Reference16 articles.

1. U.S. Army Aviation and Missile Command. Detail specification for the tank fuel crash- Resistant Ballistic-Tolerant aircraft MIL-DTL-27422D. 2007.

2. MIL-T-7378A MILITARY SPECIFICATION: TANK FUEL AIRCRAFT EXTERNAL AUXILIARY REMOVEABLE 20 OCT 1958.

3. A Study on Simplified Sloshing Impact Response Analysis for Membrane-Type LNG Cargo Containment System

4. A probabilistic assessment of design sloshing pressure time histories in LNG tanks

5. Numerical Simulation of Sloshing Test for Fuel Tank of Rotorcraft

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