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contributor authorA. G. Fabula
date accessioned2017-05-08T23:22:17Z
date available2017-05-08T23:22:17Z
date copyrightSeptember, 1964
date issued1964
identifier issn0098-2202
identifier otherJFEGA4-27255#561_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101045
description abstractLinearized theory for two-dimensional, choked-tunnel flow is developed for a vented or cavitating hydrofoil midway between infinite parallel walls, when the upper and lower free streamlines detach at an arbitrary chordwise location and at the trailing edge, respectively. Superposition of step-profile solutions gives the arbitrary-profile solution. Numerical calculations are made for two vented hydrofoils for exhaust at 30 percent chord and tunnel height-to-chord ratio of 3.5. The agreement with experiment becomes good after correction for the pressure at the test-section, static-pressure tap due to the hydrofoil and the cavity. Various aspects of the comparison for equal cavity number of choked flow with unbounded flow are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleChoked Flow About Vented or Cavitating Hydrofoils
typeJournal Paper
journal volume86
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3653173
journal fristpage561
journal lastpage567
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsHydrofoil
keywordsTunnels
keywordsPressure
keywordsChords (Trusses)
keywordsCavities AND Exhaust systems
treeJournal of Fluids Engineering:;1964:;volume( 086 ):;issue: 003
contenttypeFulltext


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