Theoretical Errors on Airborne Measurements Of: Static Pressure, Impact Temperature,air Flow Angle, Air Flow Speed

Report on a complete theory development that gives an exact calculation for all angles with irrotational flow around a sphere, the easiest shape for a nose radome which includes a few examples of axisymmetric calculations wherein four kinds of errors are approached: - static pressure and pressure coefficient, - impact temperature and pressure coefficient, - airflow angles and angle of sideslip, and - airflow speed and total pressure on radome.

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Author Nacass, Philippe
Publisher UCAR/NCAR - Library
Publication Date 1992-01-01T00:00:00
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Topic Category geoscientificInformation
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Metadata Date 2023-08-18T18:04:33.648419
Metadata Record Identifier edu.ucar.opensky::technotes:152
Metadata Language eng; USA
Suggested Citation Nacass, Philippe. (1992). Theoretical Errors on Airborne Measurements Of: Static Pressure, Impact Temperature,air Flow Angle, Air Flow Speed. UCAR/NCAR - Library. http://n2t.net/ark:/85065/d7x63m96. Accessed 23 April 2024.

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