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Subsonic sting interference on the drag of a family of slanted-base ogive-cylindersSupport interference free drag measurements on a range of slanted-base ogive-cylinders are made using the NASA Langley 13 inch Magnetic Suspension and Balance System. Comparison is made to measurements with a dummy sting support. Significant support interferences are found at most test conditions. Further comparison is made between interference free base pressures, obtained using remote telemetry, and sting cavity pressures.
Document ID
19890060294
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Britcher, Colin P. (Old Dominion University Norfolk, VA, United States)
Kilgore, W. Allen (Old Dominion Univ. Norfolk, VA, United States)
Alcorn, Charles W. (Old Dominion Univ. Norfolk, 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 89-2206
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Seattle, WA
Country: United States
Start Date: July 31, 1989
End Date: August 2, 1989
Sponsors: AIAA
Accession Number
89A47665
Funding Number(s)
CONTRACT_GRANT: NAG1-716
Distribution Limits
Public
Copyright
Other

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