Development of High-temperature Strain Gages

Development of High-temperature Strain Gages
Author: J. W. Pitts
Publisher:
Total Pages: 318
Release: 1961
Genre: Cement
ISBN:

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A summary is presented of a research program aimed at the improvement of high-temperature strain gages of the electrical resistance type. Potential ceramic and metal components were evaluated and a gage was devised that was based on these evaluations. This gage (NBS 5B) was flexible and easy to install; however, it lacked resistance stability at higher temperatures. In an attempt to minimize this deficiency, ceramic cements were developed that showed greater electrical resistivity than had been previously observed in the range 800 to 1800 degrees Fahrenheit; also, a technique was devised for increasing the resistance to ground by applying a fired-on ceramic coating to the grid of a specifically developed unbacked gage. A study was made of the cause of the erratic response of cemented gages that had not been preheated prior to use. There were strong indications that the erratic response was caused mostly by the rapid decrease in resistance that accompanied structural changes in the cement.

NBS Special Publication

NBS Special Publication
Author:
Publisher:
Total Pages: 530
Release: 1968
Genre: Weights and measures
ISBN:

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NBS Monograph

NBS Monograph
Author:
Publisher:
Total Pages: 20
Release: 1961
Genre: Physics
ISBN:

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Instrumentation Systems

Instrumentation Systems
Author: Enoch J. Durbin
Publisher: Elsevier
Total Pages: 572
Release: 2014-05-12
Genre: Technology & Engineering
ISBN: 1483222314

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Flight Testing, Volume IV: Instrumentation Systems serves as a guide to flight test instrumentation systems for establishing flight test programs. This book provides aircraft flight testers with the information required to appreciate the capabilities and limitations of the instrumentation techniques, indicating some of the many alternatives possible in flight instrumentation. It considers the systems concept in planning flight test instrumentation and functional organization of the component parts of an instrumentation system, followed by a discussion of the components of a flight data acquisition and reduction system that are organized into functional categories. Within these categories, a comparison is made between the various data collection systems and data reducing systems. The similarities, advantages, and limitations of each type of system component and significance of the fundamental properties of each device are also noted in this volume. This compilation is written primarily for persons not well-trained in electronics with special emphasis toward promoting the systems point of view in considering the problems of measurement in flight.

M

M
Author: Anthony W. Fiore
Publisher:
Total Pages: 238
Release: 1977
Genre: Reynolds number
ISBN:

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Design and Calibration of a Total-temperature Probe for Use at Supersonic Speeds

Design and Calibration of a Total-temperature Probe for Use at Supersonic Speeds
Author: David L. Goldstein
Publisher:
Total Pages: 17
Release: 1949
Genre: Probes (Electronic instruments)
ISBN:

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The results of a study of the factors involved in the design of total-temperature probes for use at supersonic speeds have been applied to the design of an instrument to be used in wind-tunnel calibrations. Tests of the probe showed that the calibration factor required in the conversion of the measured temperature to the true total temperature was 0.992 pluse or minus 0.002 for a range of Mach numbers between 1.36 and 2.01. The calibration factor was insensitive to angles of inclination relative to the air stream up to 9 degrees at a Mach number of 1.50.