The paper describes a measurement system made for registering data from the static tests of motor glider AOS-71 (the motor glider was designed in Rzeszów and Warsaw Universities of Technology). The experiment was an evidence part leading to obtaining the acceptance of the aircraft flight worthiness. The characteristic feature of the described studies was the necessity of running the strength tests in higher temperature.
A measurement system for static test of airplane structure
2014-05-01
1144530 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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