107 (2004)] that eddy current conductivity measurements can be exploited for near-surface residual stress assessment in surface-treated nickel-base superalloy components. To quanti-tatively assess the prevailing residual stress from eddy current conductivity measurements, the piezoresistivity coefficients of the material must be first determined using known exter-nal applied stresses. These calibration measurements are usually conducted on a reference specimen of the same material using cyclic uniaxial loads between 0.1 and 10 Hz, which is fast enough to produce adiabatic conditions. Therefore, the question arises whether dynamic calibration measurements can be used or not for accurately assessing the sensitivity of the eddy current method ...
Typical aero engine alloys, such as IN718, can be surface-treated by shot peening to induce near-sur...
Non-destructive measurement of residual stress at the subsurface of nickel-based alloys using eddy c...
In shot peening, design engineers typically provide the desired peening intensity or desired residua...
Recent research results indicate that eddy current conductivity measurements can be exploited for no...
Abstract Recent research results indicate that eddy current conductivity measurements can be exploit...
It is shown in this paper that, in contrast with most other materials, shot-peened nickel-base super...
Shot-peened nickel-base superalloys exhibit 1–2 % increase in apparent eddy current conduc-tivity (A...
Recently, it has been shown that shot-peened nickel-base superalloys exhibit an ap-proximately 1 % i...
Characterization of near-surface residual stress-profits on aero-engine components with high frequen...
Super Alloys, commonly used in safety-critical aerospace components, regularly impose problems when ...
To evaluate the whole residual stress profile of sub-surface processes, existing methods such as X-r...
The knowledge of residual stress profile generated by subsurface processes in aircraft turbine engin...
The knowledge of residual stress profile generated by subsurface processes in aircraft turbine engin...
An exploratory investigation was conducted to evaluate the applicability of state-of-the-art eddy cu...
This paper reports on a self‐consistent, swept frequency eddy current (SFEC) technique for character...
Typical aero engine alloys, such as IN718, can be surface-treated by shot peening to induce near-sur...
Non-destructive measurement of residual stress at the subsurface of nickel-based alloys using eddy c...
In shot peening, design engineers typically provide the desired peening intensity or desired residua...
Recent research results indicate that eddy current conductivity measurements can be exploited for no...
Abstract Recent research results indicate that eddy current conductivity measurements can be exploit...
It is shown in this paper that, in contrast with most other materials, shot-peened nickel-base super...
Shot-peened nickel-base superalloys exhibit 1–2 % increase in apparent eddy current conduc-tivity (A...
Recently, it has been shown that shot-peened nickel-base superalloys exhibit an ap-proximately 1 % i...
Characterization of near-surface residual stress-profits on aero-engine components with high frequen...
Super Alloys, commonly used in safety-critical aerospace components, regularly impose problems when ...
To evaluate the whole residual stress profile of sub-surface processes, existing methods such as X-r...
The knowledge of residual stress profile generated by subsurface processes in aircraft turbine engin...
The knowledge of residual stress profile generated by subsurface processes in aircraft turbine engin...
An exploratory investigation was conducted to evaluate the applicability of state-of-the-art eddy cu...
This paper reports on a self‐consistent, swept frequency eddy current (SFEC) technique for character...
Typical aero engine alloys, such as IN718, can be surface-treated by shot peening to induce near-sur...
Non-destructive measurement of residual stress at the subsurface of nickel-based alloys using eddy c...
In shot peening, design engineers typically provide the desired peening intensity or desired residua...