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contributor authorTetsuo Nishiyama
date accessioned2017-05-08T23:03:11Z
date available2017-05-08T23:03:11Z
date copyrightJune, 1977
date issued1977
identifier issn0098-2202
identifier otherJFEGA4-26915#311_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90050
description abstractIn order to clarify the compressibility effect, the perturbed flow field of the supercavitating hydrofoil in subsonic region is examined by a linearized technique and, as a result, the general corresponding rule of the compressible flow to the incompressible one is proposed to obtain the characteristics of the supercavitating hydrofoil. The main contents are summarized as follows: (i ) Basic relations between velocity, pressure, and sound speed are shown in subsonic liquid flow within the framework of linearization. (ii ) The correspondence of the steady, characteristics of the two and three dimensional supercavitating hydrofoils in subsonic liquid flow to ones in incompressible flow is clarified. Hence we can readily calculate the characteristics by simple correction to ones in incompressible flow. (iii ) Numerical calculations are made to show the essential differences of the compressibility effect between liquid and gas flow, and also the interrelated effect between cavitation number and Mach number on the characteristics of the supercavitating hydrofoils.
publisherThe American Society of Mechanical Engineers (ASME)
titleLinearized Theory of Supercavitating Hydrofoils in Subsonic Liquid Flow
typeJournal Paper
journal volume99
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448754
journal fristpage311
journal lastpage318
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsHydrofoil
keywordsCompressibility
keywordsPressure
keywordsMach number
keywordsSound
keywordsGas flow
keywordsCavitation AND Compressible flow
treeJournal of Fluids Engineering:;1977:;volume( 099 ):;issue: 002
contenttypeFulltext


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