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Trailing anemometer for low airspeed calibrationA propeller-type trailing airspeed anemometer system is described for low airspeed (M not exceeding 0.2) calibration which has improved accuracy and is easy to implement as compared to most methods currently in use. The trailing anemometer system consists of the trailing anemometer itself, a deployment mechanism, and an operator's control box. The trailing anemometer is a small low-drag brass body provided with tail fins for self-alignment with the airstream. The rotational speed of a small six-bladed low-inertia propeller is sensed with a miniature self-generating tachometer inside the anemometer. A very satisfactory airspeed calibration can be made with this device in which true airspeed can be measured to within 1 knot. Results from flight calibration of an aircraft and trail-back characteristics of the anemometer and cable are included. The operating speed range of the designed cable-anemometer combination is 7 to 165 knots.
Document ID
19760048993
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fisher, B. D.
(NASA Langley Research Center Hampton, VA, United States)
Stough, H. P.
(NASA Langley Research Center Hampton, VA, United States)
Kershner, D. D.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1976
Subject Category
Aircraft Instrumentation
Report/Patent Number
SAE PAPER 760461
Meeting Information
Meeting: Business Aircraft Meeting
Location: Wichita, Kan.
Start Date: April 6, 1976
End Date: April 9, 1976
Sponsors: Society of Automotive Engineers
Accession Number
76A31959
Distribution Limits
Public
Copyright
Other

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