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Evaluation of a total energy-rate sensor on a transport airplaneA sensor that measures the rate of change of total energy of an airplane with respect to the airstream has been evaluated. The sensor consists of two cylindrical probes located on the fuselage of a transport airplane, an in line acoustic filter, and a pressure sensing altitude rate transducer. Sections of this report include the sensor description and experimental configuration, frequency response tests, analytical model development, and flight test results for several airplane maneuvers. The results section includes time history comparisons between data generated by the total energy rate sensor and calculated data derived from independent sources.
Document ID
19840004096
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ostroff, A. J. (NASA Langley Research Center Hampton, VA, United States)
Hueschen, R. M. (NASA Langley Research Center Hampton, VA, United States)
Hellbaum, R. F. (NASA Langley Research Center Hampton, VA, United States)
Belcastro, C. M. (NASA Langley Research Center Hampton, VA, United States)
Creedon, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1983
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TP-2212
L-15461
NAS 1.60:2212
Accession Number
84N12164
Funding Number(s)
PROJECT: RTOP 534-04-13-54
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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