Slosh & Vibration Qualification Test for Fuel Tank of Rotorcraft

Autor: Kiwon Jang, Gui-Cheon Lee, In-Hee Hwang, Sungchan Kim, Pil-Sun Jun, Byung-Kun Ha, Jong-Won Lee, Hyun-Gi Kim, Dong-Woo Shin, Tae-Kyung Jung
Rok vydání: 2011
Předmět:
Zdroj: Journal of the Korea Institute of Military Science and Technology. 14:62-68
ISSN: 1598-9127
Popis: Rapid turning and accelerated movement of a rotorcraft leads to the slosh and vibration effect of fuel in the fuel tank. Due to the slosh load, the internal component of a fuel tank can be broken and fuel tank skin can be damaged. This is directly related to human survivability. Military specification(MIL-DTL-27422D) requires the verification of the stability of aircraft fuel tank and internal component against slosh & vibration load through the qualification test. This report shows the establishment of slosh and vibration test facility and KUH fuel tank qualification test result.
Databáze: OpenAIRE