"Quantitative assessment of the surface relief in fatigue using AFM." . . . . "80-214-1892-3" . "Brno" . "2001-06-27+02:00"^^ . . . "Quantitative assessment of the surface relief in fatigue using AFM." . . . "[0690EC87D344]" . "Proceedings International Conference on Materials Structure & Micromechanics of Fracture MSMF-3." . "Man, Ji\u0159\u00ED" . . . "Atomic force microscopy (AFM) was applied to study the early stages of fatigue damage in polycrystalline copper and stainless 316L steel. The analysis of the image formation using an AFM tip reveals the lateral distortion of the extrusions and intrusions in case of high extrusions and deep intrusions. The true extrusion height can be obtained in direct observation and the depth of intrusions using replica technique. The evolution of the shape and the height of extrusions allowed to judge the activity of the persistent slip bands (PSBs) during fatigue life."@en . . "9"^^ . "RIV/68081723:_____/01:07013100" . "Brno [CZ]" . "P(GA106/00/D055), P(GA106/01/0376), Z(AV0Z2041904)" . "Pol\u00E1k, Jaroslav" . "3"^^ . "0"^^ . "Atomic force microscopy (AFM) was applied to study the early stages of fatigue damage in polycrystalline copper and stainless 316L steel. The analysis of the image formation using an AFM tip reveals the lateral distortion of the extrusions and intrusions in case of high extrusions and deep intrusions. The true extrusion height can be obtained in direct observation and the depth of intrusions using replica technique. The evolution of the shape and the height of extrusions allowed to judge the activity of the persistent slip bands (PSBs) during fatigue life." . . . "0"^^ . . . . . "Quantitative assessment of the surface relief in fatigue using AFM."@en . "fatigue, AFM, surface relief"@en . "693775" . "3"^^ . "469;477" . "Quantitative assessment of the surface relief in fatigue using AFM."@en . "Obrtl\u00EDk, Karel" . . "Vysok\u00E9 u\u010Den\u00ED technick\u00E9 v Brn\u011B. Nakladatelstv\u00ED VUTIUM" . "RIV/68081723:_____/01:07013100!RIV/2003/AV0/A07003/N" . . . . .