Possibility of the use of the laser generation of surface acoustic waves in the blades of aircraft gas turbine engines, registration, processing and analysis of the parameters of acoustic waves to assess the possibility of determination of residual stresses.
неразрушающий контроль, лазер, напряженно-деформированное состояние, газотурбинный двигатель, non-destructive testing, laser, stress-strain state, gas turbine engine
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