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contributor authorM. G. Dunn
contributor authorC. W. Haldeman
date accessioned2017-05-08T23:47:27Z
date available2017-05-08T23:47:27Z
date copyrightDecember, 1995
date issued1995
identifier issn0098-2202
identifier otherJFEGA4-27099#653_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/115462
description abstractPhase-resolved surface pressure, and unsteady pressure measurements are reported for the first-stage blade row of the Space Shuttle Main Engine two-stage fuel-side turbine. Measurements were made at 10, 50, and 90 percent span on both the pressure and suction surfaces of the blade. Phase-resolved and unsteady heat-flux measurements are also reported.
publisherThe American Society of Mechanical Engineers (ASME)
titlePhase-Resolved Surface Pressure and Heat-Transfer Measurements on the Blade of a Two-Stage Turbine
typeJournal Paper
journal volume117
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2817318
journal fristpage653
journal lastpage658
identifier eissn1528-901X
keywordsPressure
keywordsHeat transfer
keywordsMeasurement
keywordsTurbines
keywordsBlades
keywordsHeat flux
keywordsPressure measurement
keywordsFuels
keywordsSuction AND Engines
treeJournal of Fluids Engineering:;1995:;volume( 117 ):;issue: 004
contenttypeFulltext


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