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Methods and results of boundary layer measurements on a gliderBoundary layer measurements were carried out on a glider under natural conditions. Two effects are investigated: the effect of inconstancy of the development of static pressure within the boundary layer and the effect of the negative pressure difference in a sublaminar boundary layer. The results obtained by means of an ion probe in parallel connection confirm those results obtained by means of a pressure probe. Additional effects which have occurred during these measurements are briefly dealt with.
Document ID
19780016142
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
Nes, W. V. (NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-75294
Accession Number
78N24085
Funding Number(s)
CONTRACT_GRANT: NASW-2790
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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