NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Damage Tolerance and Reliability of Turbine Engine ComponentsA formal method is described to quantify structural damage tolerance and reliability in the presence of multitude of uncertainties in turbine engine components. The method is based at the materials behavior level where primitive variables with their respective scatters are used to describe that behavior. Computational simulation is then used to propagate those uncertainties to the structural scale where damage tolerance and reliability are usually specified. Several sample cases are described to illustrate the effectiveness, versatility, and maturity of the method. Typical results from these methods demonstrate that the methods are mature and that they can be used for future strategic projections and planning to assure better, cheaper, faster products for competitive advantages in world markets. These results also indicate that the methods are suitable for predicting remaining life in aging or deteriorating structures.
Document ID
19990064547
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
Authors
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1998
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: SC.78: Qualification of Life Extension Schemes for Engine Components
Location: Corfu
Country: Greece
Start Date: October 5, 1998
End Date: October 9, 1998
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available