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Measurement of static pressure on aircraftExisting data on the errors involved in the measurement of static pressure by means of static-pressure tubes and fuselage vents are presented. The errors associated with the various design features of static-pressure tubes are discussed for the condition of zero angle of attack and for the case where the tube is inclined to flow. Errors which result from variations in the configuration of static-pressure vents are also presented. Errors due to the position of a static-pressure tube in the flow field of the airplane are given for locations ahead of the fuselage nose, ahead of the wing tip, and ahead of the vertical tail fin. The errors of static-pressure vents on the fuselage of an airplane are also presented. Various methods of calibrating static-pressure installations in flight are briefly discussed.
Document ID
19930092348
Document Type
Other
Authors
Gracey, William
Date Acquired
September 6, 2013
Publication Date
January 1, 1958
Report/Patent Number
NACA-TR-1364
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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