Possibilities and Methods of In Flight Loading Measurements
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F11%3APU95249" target="_blank" >RIV/00216305:26210/11:PU95249 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Possibilities and Methods of In Flight Loading Measurements
Original language description
This article provides information about in-flight measurement of a small sport aircraft. Firstly the strain gauges were installed into the wing structure and then the calibration procedures were done. After the calculation of strain gauge coefficients the equations for calculating of bending moments and other variables were established. The data acquisition system was installed into the aircraft for measurement responses from strain gauges and other variables as speed, altitude, load factor and temperature. Many flights were performed with this way equipped aircraft and after that the recorded data were analyzed and those results were compared with the calculation and with the static strength tests performed before.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů