ANALYTICAL AND EXPERIMENTAL STRESS FIELD IMAGE IN A RIVET JOINT
THE CAUSE ANALYSIS OF THE AIRCRAFT ENGINE TURBINE BLADES FAILURE
PHYSICAL AND CHEMICAL, PHENOMENA AT THE CRACK FRONT II. Composite materials, pressures and stresses
NON-DESTRUCTIVE DIAGNOSTICS - PHYSICS FOUNDATIONS - PERSPECTIVES - SELECTED ISSUES
I-22 IRYDA AIRCRAFT WING SPAR DIAGNOSTIC. SELECTED ISSUES
INFLUENCE OF THE DESIGN AND MANUFACTURING PROCESSES ON TO COMPRESSOR LIFE CYCLE OF K-15 ENGINE
IN-LOCK COOPERATION BETWEEN THE BLADE AND THE DISC OF THE COMPRESSOR OF THE AIRCRAFT TURBINE ENGINE
Comparative Tests of Ultrahigh Steels N18K9M5TPr and 30HGSNA
Selected Magnetic Properties of Precipitation Hardened Martensite Steel of N18K9M5Pr Sort