Verification of reliability of numerical analysis by comparison with actual crash impact test of rotorcraft fuel tank
Author:
Affiliation:
1. Department of Aircraft Systems, Aeronautics Research and Development Head Office, Korea Aerospace Research Institute, Yuseong-gu, Daejeon, Republic of Korea
Publisher
Informa UK Limited
Subject
Industrial and Manufacturing Engineering,Mechanical Engineering,Transportation
Link
https://www.tandfonline.com/doi/pdf/10.1080/13588265.2019.1617659
Reference11 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. Simulation and Analysis of Crashworthiness of Fuel Tank for Helicopters
3. Crushing Simulation of a Partially Filled Fuel Tank Beyond Failure
4. Simulation of Fuel Tank Filling using a Multi-material Euler Solver with Multiple Adaptive Domains
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1. Verification test of the structural integrity of an external fuel tank for aircraft under slosh and vibration conditions;International Journal of Crashworthiness;2024-02-13
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