THE ESTIMATION OF DYNAMIC STRESS IN ACOUSTICALY EXITED STRUCTURES
TEMPERATURE MEASUREMENTS AND TURBINE BLADE STRENGTH QUALIFICATION IN K-15 AND K-16 ENGINES
THE MEASUREMENT SYSTEM UNILOG 2500 IN STRUCTUAL AND COMPONENT TEST LABORATORY'S PRACTICE
UNCERTAINITY IN MEASUREMENT, ON THE BASIS OF MEASUREMENT OF FORCE
DIAGNOSTIC SYSTEM FOR AIRCRAFT TURBINE ENGINES
FATIGUE TEST OF WING STRUCTURE
INSTITUTE OF AVIATION STRUCTURAL AND COMPONENT LABORATORY
NON-DESTRUCTIVE DIAGNOSTICS - PHYSICS FOUNDATIONS - PERSPECTIVES - SELECTED ISSUES
JET TURBINE ENGINE LOAD MEASURMENTS AND ANALYSIS
PRE-STOCHASTIC MODELS OF COMPUTATIONAL PROBABILITY
MECHANICAL AND THERMAL LOADS OF TURBINE JET ENGINE MONITORING POSSIBILITIES DURING OPERATION
I-22 IRYDA AIRCRAFT WING SPAR DIAGNOSTIC. SELECTED ISSUES
MAXIMUM LOADING CAPACITY AND LOW CYCLING FATIGUE TESTS OF JET ENGINE ROTOR ELEMENTS
FRACTOGRAFIC ANALYSES AS A TOOL TO DETERMINATION FATIGUE LIFE OF A WING STRUCTURE
INFLUENCE OF THE DESIGN AND MANUFACTURING PROCESSES ON TO COMPRESSOR LIFE CYCLE OF K-15 ENGINE
THE METHOD OF DETERMINATION THE SERVICE LIFE OF LANDING GEAR BASED ON TESTS AND SERVICE DUTY
IN-LOCK COOPERATION BETWEEN THE BLADE AND THE DISC OF THE COMPRESSOR OF THE AIRCRAFT TURBINE ENGINE