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    Material Property Studies of Two High-Pressure Turbine Rotors for Remaining Life Assessment 

    Source: Journal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 001:;page 19
    Author(s): V. P. Swaminathan; R. Viswanathan; C. P. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A remaining life assessment study was performed on two no-bore HP rotors after 169,000 hours of operation. These rotors were manufactured from 1CrMoV (ASTM A470, Class 8) steel. Southwest ...
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    Temperature Estimation and Life Prediction of Turbine Blades Using Post-Service Oxidation Measurements 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004:;page 922
    Author(s): V. P. Swaminathan; J. M. Allen; G. L. Touchton
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The depth of internal oxidation and nitridation from the surface of the 16 cooling holes in a first-stage turbine blade was measured by optical microscopy after 32,000 hours of service. Maximum ...
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    Life Assessment of an HP-IP Rotor Under Creep Service Conditions 

    Source: Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 002:;page 237
    Author(s): V. P. Swaminathan; N. S. Cheruvu; A. Saxena
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A CrMoV high and intermediate-pressure (HP-IP) rotor exhibited in-service cracking in the blade groove walls. Cracks initiated from a notch and propagated under creep conditions to a depth of ...
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