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Liquid Sloshing in a Spherical Tank Filled to an Arbitrary DepthDynamic analysis of liquid in a spherical tank with applications to trajectory failure and loss of control in missile and rocket flight
Document ID
19630003755
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chu, W.-H. (Southwest Research Inst. San Antonio, TX, United States)
Date Acquired
September 2, 2013
Publication Date
December 15, 1962
Subject Category
Physics, General
Accession Number
63N13631
Funding Number(s)
CONTRACT_GRANT: NAS8-1555
CONTRACT_GRANT: DA-23-072-ORD-1251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET FLIGHT
FLUID MECHANICS
SPHERICAL TANK
LIQUID PROPELLANT
TRAJECTORY CONTROL
LIQUID SLOSHING
MISSILE

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