NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Porous Plug for Reducing Orifice Induced Pressure Error in AirfoilsA porous plug is provided for the reduction or elimination of positive error caused by the orifice during static pressure measurements of airfoils. The porous plug is press fitted into the orifice, thereby preventing the error caused either by fluid flow turning into the exposed orifice or by the fluid flow stagnating at the downstream edge of the orifice. In addition, the porous plug is made flush with the outer surface of the airfoil, by filing and polishing, to provide a smooth surface which alleviates the error caused by imperfections in the orifice. The porous plug is preferably made of sintered metal, which allows air to pass through the pores, so that the static pressure measurements can be made by remote transducers.
Document ID
19890003470
Acquisition Source
Langley Research Center
Document Type
Other - Patent
External Source(s)
LAR-13569-1
Authors
Elizabeth B Plentovich
(Langley Research Center Hampton, United States)
Blair B Gloss
(Langley Research Center Hampton, United States)
John W Eves
(Langley Research Center Hampton, United States)
John P Stack
(Langley Research Center Hampton, United States)
Date Acquired
August 14, 2013
Publication Date
September 13, 1988
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Instrumentation And Photography
Accession Number
89N12841
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,770,032
Patent Application
US-PATENT-APPL-SN-010943
No Preview Available