The evaluation of the RFC/NDE System has produced capability characteristics in the format of â vs. a or apparent cracksize vs. actual cracksize. Although crack sizing has long been a major concern of NDE practitioners and theoreticians, the analysis procedure which permits straightforward conversion of these â vs. a to POD vs. a, or Probability of Detection vs. cracksize, is a recent development [1]. This paper will compare these two descriptions of NDE system capability by comparing their influence on the Retirement for Cause (RFC) process
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
Probability of detection (POD) analysis is used in assessing reliably detectable flaw size in nondes...
AbstractTotal fatigue life is traditionally composed of the time to crack initiation plus the time f...
The evaluation of the RFC/NDE System has produced capability characteristics in the format of â vs. ...
The RFC/NDE System comprises automated eddy current and ultrasonic inspection stations developed by ...
Current nondestructive evaluation techniques generally do not produce identical indications when app...
The damage tolerance approach to structural safety is based on the predicted growth of the “largest”...
The goal of this paper is to review the statistical methods used in the aerospace industries to eval...
The Phase I Reliability Test was successfully conducted on the RFC/NDE Inspection System in November...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
The demand for quantified nondestructive evaluation (NDE) has increased significantly with increasin...
Major cost savings are possible through life extension of high-cost jet engine components until dama...
This paper presents results of Monte Carlo simulation of the Retirement-for-Cause (RFC) engine maint...
Nondestructive evaluation (NDE) is widely used in the aerospace industry during scheduled maintenanc...
I would like to present some ideas regarding the current stat us of fatigue crack NOE, where the fie...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
Probability of detection (POD) analysis is used in assessing reliably detectable flaw size in nondes...
AbstractTotal fatigue life is traditionally composed of the time to crack initiation plus the time f...
The evaluation of the RFC/NDE System has produced capability characteristics in the format of â vs. ...
The RFC/NDE System comprises automated eddy current and ultrasonic inspection stations developed by ...
Current nondestructive evaluation techniques generally do not produce identical indications when app...
The damage tolerance approach to structural safety is based on the predicted growth of the “largest”...
The goal of this paper is to review the statistical methods used in the aerospace industries to eval...
The Phase I Reliability Test was successfully conducted on the RFC/NDE Inspection System in November...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
The demand for quantified nondestructive evaluation (NDE) has increased significantly with increasin...
Major cost savings are possible through life extension of high-cost jet engine components until dama...
This paper presents results of Monte Carlo simulation of the Retirement-for-Cause (RFC) engine maint...
Nondestructive evaluation (NDE) is widely used in the aerospace industry during scheduled maintenanc...
I would like to present some ideas regarding the current stat us of fatigue crack NOE, where the fie...
The life prediction of critical gas turbine engine components is carried out using a bank of laborat...
Probability of detection (POD) analysis is used in assessing reliably detectable flaw size in nondes...
AbstractTotal fatigue life is traditionally composed of the time to crack initiation plus the time f...