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contributor authorMihai Arghir
date accessioned2017-05-09T00:23:33Z
date available2017-05-09T00:23:33Z
date copyrightOctober, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26973#1144_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135650
description abstractThe authors are grateful for this experimental validation of the negative direct static stiffness of choked annular seals. For performing our own calculations, the mentioned conditions were supplemented by some additional assumptions that are somewhat usual for straight annular seals, namely, an imposed inlet pressure drop coefficient ζinlet and an exit recovery coefficient ζexit=1 (complete pressure recovery). The rotation speed was ω=0, and the flow regime was considered as being nonisothermal with adiabatic walls and Tinlet=20°C. Moody’s friction factor was used with the possibility of bridging transition between laminar and turbulent flow. The employed grid had 16 equally spaced cells in the axial direction and 32 in the circumferential one (Fig. 1).
publisherThe American Society of Mechanical Engineers (ASME)
titleClosure to “Discussion of ‘The Lomakin Effect in Annular Gas Seals Under Choked Flow Conditions’ ” (2007, ASME J. Eng. Gas Turbines Power, 129 , p. 1143)
typeJournal Paper
journal volume129
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2718219
journal fristpage1144
identifier eissn0742-4795
keywordsFlow (Dynamics) AND Gas turbines
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 004
contenttypeFulltext


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