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Reflection type skin friction meterA housing block is provided having an upper surface conforming to the test surface of a model or aircraft. An oil film is supplied upstream of a transparent wedge window located in this upper surface by an oil pump system located external to the housing block. A light source located within the housing block supplies a light beam which passes through this transparent window and is reflected back through the transparent window by the upper surface of the oil film to a photo-sensitive position sensor located within the housing. This position sensor allows the slope history of the oil film caused by and aerodynamic flow to be determined. The skin friction is determined from this slope history. Internally located mirrors augment and sensitize the reflected beam as necessary before reaching the position sensor. In addition, a filter may be provided before this sensor to filter the beam.
Document ID
19930009086
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Bandyopadhyay, Promode R.
(AS&M, Inc. Hampton, VA., United States)
Weinstein, Leonard M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
January 12, 1993
Subject Category
Aerodynamics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-742238
Patent Number: NASA-CASE-LAR-14520-1-SB
Patent Number: US-PATENT-5,178,004
Accession Number
93N18275
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-14520-1-SB|US-PATENT-5,178,004
Patent Application
US-PATENT-APPL-SN-742238
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