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Hydrostatic Stability Of The Liquid Vapor Interface In A Low Acceleration Field Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Hydrostatic Stability Of The Liquid Vapor Interface In A Low Acceleration Field book. This book definitely worth reading, it is an incredibly well-written.
Author : William J. Masica,Joseph D. Derdul,Donald A. Petrash
Publisher : Unknown
Page : 24 pages
File Size : 54,5 Mb
Release : 1964
Category : Gas-liquid interfaces
ISBN : UIUC:30112106866996
Author : William J. Masica,Donald A. Petrash,Edward W. Otto
Publisher : Unknown
Page : 24 pages
File Size : 46,8 Mb
Release : 1964
Category : Gas-liquid interfaces
ISBN : UIUC:30112106866020
Author : Anonim
Publisher : Unknown
Page : 342 pages
File Size : 52,6 Mb
Release : 1967
Category : Electronic
ISBN : MINN:319510008460871
Author : Raouf A. Ibrahim
Publisher : Cambridge University Press
Page : 986 pages
File Size : 44,9 Mb
Release : 2005-05-19
Category : Technology & Engineering
ISBN : 1139444131
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 : Anonim
Publisher : Unknown
Page : 344 pages
File Size : 42,5 Mb
Release : 1969
Category : Weights and measures
ISBN : UCAL:B4112699
Author : Anonim
Publisher : Unknown
Page : 334 pages
File Size : 51,9 Mb
Release : 1968
Category : Hydraulic engineering
ISBN : PSU:000003429051
Author : United States. National Bureau of Standards
Publisher : Unknown
Page : 342 pages
File Size : 41,8 Mb
Release : 1969
Category : Hydraulic engineering
ISBN : UOM:39015095088137
Author : United States. National Bureau of Standards
Publisher : Unknown
Page : 696 pages
File Size : 49,8 Mb
Release : 1968
Category : Hydraulic engineering
ISBN : UIUC:30112008456433
Author : United States. National Bureau of Standards
Publisher : Unknown
Page : 1046 pages
File Size : 49,7 Mb
Release : 1968
Category : Hydraulic engineering
ISBN : OSU:32435062361381
Author : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher : Unknown
Page : 1152 pages
File Size : 49,6 Mb
Release : 1965
Category : Aeronautics
ISBN : STANFORD:36105024714839
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher : Unknown
Page : 1156 pages
File Size : 53,7 Mb
Release : 1964
Category : Aeronautics
ISBN : CORNELL:31924057848818
Author : Joseph D. Derdul,Lynn S. Grubb,Donald A. Petrash
Publisher : Unknown
Page : 28 pages
File Size : 41,5 Mb
Release : 1966
Category : Liquid propellant rockets
ISBN : UIUC:30112106867515
Author : Yvonne Chen
Publisher : Cuvillier Verlag
Page : 286 pages
File Size : 45,8 Mb
Release : 2015-06-08
Category : Technology & Engineering
ISBN : 9783736980105
The knowledge of behavior of liquids with free surfaces to their surrounding gaseous phase in compensated gravity is essential to the development of tank systems for spacecrafts. In microgravity, the liquid behavior is dominated by capillary forces, which are used to position and redistribute liquid propellant in a desired way for the mission. The body forces occurring due to residual accelerations, which can be caused by spin during the ballistic flight phases, force the liquid to reorient towards a new equilibrium state of the free surface. Due to spin the liquid is driven away from the tank outlet and located along tank walls in partially filled tanks. To assure enough liquid fuel over the tank outlet, so-called Propellant Management Devices (PMD’s), are employed. A PMD is a static, usually metal structure, which either provides a passage way for a liquid in microgravity or stores a certain amount of liquid at a desired location. Some PMD’s are designed to be refillable in periods of microgravity due to openings in the outer housing or by a housing composed of perforated metallic sheets. These reservoirs are refilled in periods of compensated gravity in order to provide the required amount of liquid fuel for attitude control or other maneuverings. Relatively large disturbances, such as lateral accelerations and spin, can drive the liquid fuel out of the reservoir, resulting in malfunction of the device. During spilling, gas enters the device such that only a residual amount of liquid propellant can be kept in the reservoir. Moreover, the connection to the bulk liquid in the tank may be interrupted such that refilling of the reservoir is disrupted. Hence, a PMD with two parallel disks forming the inlet and a venting tube at the topmost point of the outer housing shall be designed such that its refillable structure is only filled with liquid without any gas or vapor being easily trapped during operations.
Author : Anonim
Publisher : Unknown
Page : 188 pages
File Size : 48,5 Mb
Release : 1966
Category : Astronautics
ISBN : STANFORD:36105113772870
Author : Anonim
Publisher : Unknown
Page : 972 pages
File Size : 45,7 Mb
Release : 1964
Category : Aeronautics
ISBN : UIUC:30112106768325
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.