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Drag measurements on a modified prolate spheroid using a magnetic suspension and balance systemLow-speed wind tunnel drag force measurements were taken on a modified prolate spheroid free of support interference. This body was tested at zero incidence in the NASA Langley 13 inch Magnetic Suspension and Balance System. This shape was one of two bodies tested to determine the drag force measuring capabilities of the 13 inch MSBS. In addition, support interference on this shape at zero incidence was quantified by using a dummy sting. The drag force calibrations and wind-on repeatability data make it possible to assess the drag force measuring capabilities of the 13 inch MSBS. Comparisons with and without the sting showed differences in the drag coefficients with the dummy sting case resulting in lower drag coefficients.
Document ID
19890038141
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dress, David A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 89-0648
Accession Number
89A25512
Distribution Limits
Public
Copyright
Other

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