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Sensitivity Study of the Wall Interference Correction System (WICS) for Rectangular TunnelsAn off-line version of the Wall Interference Correction System (WICS) has been implemented for the NASA Langley National Transonic Facility. The correction capability is currently restricted to corrections for solid wall interference in the model pitch plane for Mach numbers less than 0.45 due to a limitation in tunnel calibration data. A study to assess output sensitivity to measurement uncertainty was conducted to determine standard operational procedures and guidelines to ensure data quality during the testing process. Changes to the current facility setup and design recommendations for installing the WICS code into a new facility are reported.
Document ID
20010011089
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Walker, Eric L.
(NASA Langley Research Center Hampton, VA United States)
Everhart, Joel L.
(NASA Langley Research Center Hampton, VA United States)
Iyer, Venkit
(Lockheed Martin Corp. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA Paper 2001-0159
Report Number: AIAA Paper 2001-0159
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 8, 2001
End Date: January 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available