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Chapter 4: TransducersThe use of transducers in the measuring channels of flight test instrumentation systems is discussed. Emphasis is placed on transducers with an electrical output. The physical effects used for producing the electrical outputs are defined. Diagrams of the various types of transducers are included to show the operating principles.
Document ID
19740017824
Acquisition Source
Legacy CDMS
Document Type
Contribution to a larger work
External Source(s)
https://www.sto.nato.int/publications/AGARD/AGARD-AG-160-VOL-1/AG-160-01-05chap04.pdf
Authors
L H Weirather (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 7, 2013
Publication Date
April 1, 1974
Publication Information
Publication: AGARD Flight Test Instrumentation Series, Volume 1: Basic Principles of Flight Test Instrumentation Engineering
Publisher: North Atlantic Treaty Organization
Volume: AGARD-AG-160-VOL-1
Subject Category
Instrumentation And Photography
Report/Patent Number
AGARDOGRAPH-160-VOL-1
AGARD-AG-160-VOL-1
Accession Number
74N25937
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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IDRelationTitle19740017820Collected WorksAGARD Flight Test Instrumentation Series, Volume 1: Basic Principles of Flight Test Instrumentation Engineering
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