Some Studies of Liquid Rotation and Vortexing in Rocket Propellant Tanks PDF Download
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Author:
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Category : Liquid propellant rockets
Languages : en
Pages : 42
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Author:
Publisher:
ISBN:
Category : Liquid propellant rockets
Languages : en
Pages : 42
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Author: H. Norman Abramson
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Category :
Languages : en
Pages : 1
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Author: H. Norman Abramson
Publisher:
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Category :
Languages : en
Pages : 35
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Author:
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Category :
Languages : en
Pages : 540
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Author: United States. National Bureau of Standards
Publisher:
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Category : Hydraulic engineering
Languages : en
Pages : 952
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Author:
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ISBN:
Category : Science
Languages : en
Pages : 236
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Author:
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Category : Weights and measures
Languages : en
Pages : 234
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Author: Raouf A. Ibrahim
Publisher: Cambridge University Press
ISBN: 9781139444132
Category : Technology & Engineering
Languages : en
Pages : 986
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Book Description
The problem of liquid sloshing in moving or stationary containers remains of great concern to aerospace, civil, and nuclear engineers; physicists; designers of road tankers and ship tankers; and mathematicians. Beginning with the fundamentals of liquid sloshing theory, this book takes the reader systematically from basic theory to advanced analytical and experimental results in a self-contained and coherent format. The book is divided into four sections. Part I deals with the theory of linear liquid sloshing dynamics; Part II addresses the nonlinear theory of liquid sloshing dynamics, Faraday waves, and sloshing impacts; Part III presents the problem of linear and nonlinear interaction of liquid sloshing dynamics with elastic containers and supported structures; and Part IV considers the fluid dynamics in spinning containers and microgravity sloshing. This book will be invaluable to researchers and graduate students in mechanical and aeronautical engineering, designers of liquid containers, and applied mathematicians.
Author: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C.
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Category :
Languages : en
Pages : 1
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Contents: Mercury Condenser Research and Development, by A. Koestel and J.J. Reinmann Pressure Drop in Two-Phase Flow, by C. Baroczy and J. Sells Snap-8 Radiator Development, by J.R. Payne Summary of Mercury Condensing Work, by J. Neustein and L. Hays Aeronatucal Systems Division Programs in Mercury Condensing, by Lloyd M. HedgepethAD270 8839N1 AD-270 884Div. 10, 9U (TISTA/SEB) OTS price $1.00 National Aeronautics and Space Administration, Washington, D.C. SOME STUDIES OF LIQUID ROTATION AND VORTEXING IN ROCKET PROPELLANT TANKS, by H. Norman Abramson, Wen-Hwa Chu and others. Jan 62, 35p. incl. illus. 16 refs. (NASA Technical note D-1212) (In cooperation with Southwest Research Inst., San Antonio, tex.) Unclassified reportAlso available from NASA, Wash. 25, D.C., as NASA Technical note D-1212. DESCRIPTORS: (*Liquid rocket propellants in *Propellant tanks, Motion, Rotation, Vortices, Dynamics, Drainage, Fluid flow, Test, Theory.) (Fuel tanks, Configuration, Design.) Identifiers: Sloshing. Experimental and theoretical studies were performed on vortex formation while draining fluid from cylindrical tanks, and related liquid dynamic behavior. The experimental studies are largely visual, through motion picture films, but even so reveal many interesting details of vortex formation and behavior, and also include some data on time required for draining with various fluids, tank bottom shapes, and slosh and vortex suppression devices. An analytical study of vortex formation in cylindrical tanks is also presented in an attempt to understand and delineate better the flow mechanisms involved. (Author).
Author: Irving E. Sumner
Publisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 28
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