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contributor authorJehanzeb Masud
contributor authorFarooq bin Akram
date accessioned2017-05-09T00:38:19Z
date available2017-05-09T00:38:19Z
date copyrightMarch, 2010
date issued2010
identifier issn0098-2202
identifier otherJFEGA4-27411#034502_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143529
description abstractIn this paper we present a methodology for adjustment of subsonic compensation characteristics of an aerodynamic-compensation Pitot tube. This methodology is based on manipulation of a Pitot tube profile (shape) downstream of the static pressure port such that its subsonic characteristics are modified while the supersonic characteristics remain unchanged. Due to this “rear-body” shape adjustment, complete redesign of a developed or in service Pitot tube is not required. We have used computational fluid dynamics tools in the analysis and design refinement of a Pitot tube by rear-body shape adjustment. The complete Mach number regime (M<2) has been computationally analyzed for three different rear-body profiles. The results of our study indicate that significant variation in subsonic compensation characteristics of a Pitot tube is possible by this method.
publisherThe American Society of Mechanical Engineers (ASME)
titleAdjustment of Aerodynamic-Compensation Characteristics of a Pitot Tube by Rear-Body Shape Manipulation
typeJournal Paper
journal volume132
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4001156
journal fristpage34502
identifier eissn1528-901X
treeJournal of Fluids Engineering:;2010:;volume( 132 ):;issue: 003
contenttypeFulltext


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