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Development and Characterization of a Low-Pressure Calibration System for Hypersonic Wind TunnelsMinimization of uncertainty is essential for accurate ESP measurements at very low free-stream static pressures found in hypersonic wind tunnels. Statistical characterization of environmental error sources requires a well defined and controlled calibration method. A calibration system has been constructed and environmental control software developed to control experimentation to eliminate human induced error sources. The initial stability study of the calibration system shows a high degree of measurement accuracy and precision in temperature and pressure control. Control manometer drift and reference pressure instabilities induce uncertainty into the repeatability of voltage responses measured from the PSI System 8400 between calibrations. Methods of improving repeatability are possible through software programming and further experimentation.
Document ID
20040008261
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Green, Del L.
(NASA Langley Research Center Hampton, VA, United States)
Everhart, Joel L.
(NASA Langley Research Center Hampton, VA, United States)
Rhode, Matthew N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA Paper 2004-0600
Meeting Information
Meeting: 42nd AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 5, 2004
End Date: January 8, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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