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contributor authorK. Bammert
contributor authorB. Ahmadi
date accessioned2017-05-08T23:04:42Z
date available2017-05-08T23:04:42Z
date copyrightJuly, 1978
date issued1978
identifier issn1528-8919
identifier otherJETPEZ-26742#432_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/90975
description abstractThe transformation of energy in the stages of high-reaction axial compressors can be considerably increased if the rotor blading consists of tandem cascades. This also involves aerodynamically higher loading of the stator cascades deflecting the flow. The behavior of the base, mean, and tip sections impulse cascades of the stator of a multi-stage axial compressor designed on this basis was examined in a two-dimensional cascade wind tunnel. The results of these investigations are reported and discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleInvestigations on Impulse Blade Cascades with Medium Deflection
typeJournal Paper
journal volume100
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446375
journal fristpage432
journal lastpage438
identifier eissn0742-4795
keywordsBlades
keywordsDeflection
keywordsImpulse (Physics)
keywordsStators
keywordsCompressors
keywordsCascades (Fluid dynamics)
keywordsFlow (Dynamics)
keywordsEnergy transformation
keywordsWind tunnels AND Rotors
treeJournal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 003
contenttypeFulltext


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