Comparison of Propellant Sloshing Parameters Obtained from Model and Full-size Centaur Liquid-oxygen Tanks PDF Download
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Author: Andrew J. Stofan
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Category :
Languages : en
Pages : 20
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Author: Andrew J. Stofan
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Category : Government publications
Languages : en
Pages : 1086
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Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1038
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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Category : Aeronautics
Languages : en
Pages : 954
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Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
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Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
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Category : Shock (Mechanics)
Languages : en
Pages : 748
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Category : Science
Languages : en
Pages : 1014
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Author: Thom A. Coney
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Category : Liquids
Languages : en
Pages : 28
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An experiment was conducted to measure the natural lateral sloshing frequency of liquids in oblate spheroidal tanks. The eccentricities of the tanks used were 0, 0.68, and 0.8. The liquids chosen exhibited 0 [degree] static contact angles on the container walls. Tests were conducted under both reduced-and normal-gravity conditions. Resulting Bond numbers ranged from 5 to 927. The data were compared with low and high Bond number theory and with the results of previous studies.
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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ISBN:
Category : Aeronautics
Languages : en
Pages : 2084
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