Experimental Methodological Investigations of Sloshing-Induced Mass Transfer Coefficients for Aircraft Tanks

What is it about?

The present work investigates the role of sloshing in the pressure drop that is expected in cryogenic hydrogen tanks that potentially will serve in the next generation aircraft. A comprehensive understanding of the physics causing pressure drop following tank acceleration caused by landing, gusts , taxiing will play a fundamental role in the design of the tanks.

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