Dynamic Influence of Propellant Sloshing Estimation Using Hybrid: Mechanical Analogy and CFD-Reference-Cited by-同舟云学术

Dynamic Influence of Propellant Sloshing Estimation Using Hybrid: Mechanical Analogy and CFD

Published:2009 Issue:177 Volume:52 Page:144-151
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

DONG Kai,QI Naiming,WANG Xianlu,CHEN Jiabao

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/52/177/52_177_144/_pdf

Reference25 articles.

1. 1) Jones, E. M.: The First Lunar Landing: Mission Time 102:38:20, Apollo-11 Lunar Surface Journal, 2008. http://www.hq.nasa.gov/office/pao/History/alsj/a11/a11.landing.html.

2. 2) Falcon-1 Data Sheet, SpaceX, 2008. http://www.spacex.com/falcon1.php.

3. 3) Brooks, G. W.: Techniques for Simulation and Analysis of Shock and Vibration Environments of Space Flight Systems, ASME Colloquium on Experimental Techniques in Shock and Vibration, 1962.

4. 5) Silverman, S. and Abramson, H. N.: Lateral Sloshing in Moving Containers, NASA SP-106, 1966.

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