Calibration of the NCAR Sabreliner Research Static Pressure Source With a Trailing Cone Assembly

Trailing cone results verify that pressure corrections for the NCAR Sabreliner derived from tower flyby data can be extrapolated to higher Mach numbers and higher altitudes with valid results. Residual static pressure errors are small, on the order of 0.1-0.3 mb, corresponding to altitude errors of 20-30 ft for altitudes of 15,000-39,000 ft and Mach numbers of 0.59-0.76.

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Bounding Box North Lat N/A
Bounding Box South Lat N/A
Bounding Box West Long N/A
Bounding Box East Long N/A
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Spatial Resolution N/A
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Copyright Author(s). This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
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Resource Support Email opensky@ucar.edu
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Metadata Contact Email opensky@ucar.edu
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Author Brown, E.
Publisher UCAR/NCAR - Library
Publication Date 1985-01-01T00:00:00
Digital Object Identifier (DOI) Not Assigned
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Resource Version N/A
Topic Category geoscientificInformation
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Metadata Date 2023-08-18T18:05:31.421449
Metadata Record Identifier edu.ucar.opensky::technotes:363
Metadata Language eng; USA
Suggested Citation Brown, E.. (1985). Calibration of the NCAR Sabreliner Research Static Pressure Source With a Trailing Cone Assembly. UCAR/NCAR - Library. http://n2t.net/ark:/85065/d7rx9bg3. Accessed 21 December 2024.

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