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Selection and static calibration of the Marsh J1678 pressure gaugeDuring the experimental testing of the ultralight, it was determined that a pressure gauge would be required to monitor the simulated flight loads. After analyzing several factors, which are indicated in the discussion section of this report, the Marsh J1678 pressure gauge appeared to be the prominent candidate for the task. However, prior to the final selection, the Marsh pressure gauge was calibrated twice by two different techniques. As a result of the calibration, the Marsh gauge was selected as the appropriate measuring device during the structural testing of the ultralight. Although, there are commerical pressure gauges available on the market that would have proven to be more efficient and accurate. However, in order to obtain these characteristics in a gauge, one has to pay the price on the price tag, and this value is an exponential function of the degree of accuracy efficiency, precision, and many other features that may be designed into the gauge. After analyzing the extent of precision and accuracy that would be required, a more expensive gauge wouldn't have proven to be a financial benefit towards the outcome of the experiment.
Document ID
19930020590
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Oxendine, Charles R.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Smith, Howard W.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: The Ultra Light Aircraft Testing
Subject Category
Instrumentation And Photography
Accession Number
93N29779
Funding Number(s)
CONTRACT_GRANT: NAG1-345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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