Prediction of Highly Dynamic Airborne Tank Fuel Sloshing and Impact Effects-Reference-Cited by-同舟云学术

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Prediction of Highly Dynamic Airborne Tank Fuel Sloshing and Impact Effects

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Baeten André¹,Stern Dirk¹

Affiliation:

1. LFK Lenkflugkoerpersysteme GmbH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-658

Reference4 articles.

1. Pressure-impulse theory for liquid impact problems

2. 15Sutmann, G., Classical Molecular Dynamics - in Lecture Notes of Quantum Simulations of Complex Many-Body Systems: FromTheory to Algorithms, Tech. Report, John von Neumann Institute for Computing (NTC), Complex Atomistic Modellingand SimulationResearch Center,Juelich,Germany,2002

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1. Lagrange-based Modeling and Testing of Composite Structure Impact Dynamics;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02

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