Skip to main content
Log in

A software tool to design thermal barrier coatings: a technical note

  • Technical Notes
  • Published:
Journal of Thermal Spray Technology Aims and scope Submit manuscript

Abstract

This paper summarizes work completed for a NASA Phase ISBIR program that demonstrated the feasi-bility of developing a software tool to aid in the design of thermal barrier coating (TBC) systems. Toward this goal, three tasks were undertaken and completed. Task 1 involved the development of a database con-taining the pertinent thermal and mechanical property data for the top coat, bond coat, and substrate materials that constitute a TBC system. Task 2 involved the development of an automated setup program for generating two-dimensional finite-element analysis (FEA) models of TBC systems. Most importantly, task 3 involved the generation of a rule base to aid in the design of a TBC system. These rules were based on a factorial design of experiments involving FEA results and were generated using a Yates analysis. A previous study had indicated the suitability and benefit of applying FEA to perform computer-based ex-periments to decrease but not eliminate physical experiments on TBCs. This program expanded on these findings by developing a larger knowledge base and a procedure to extract rules to aid in the TBC design.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. W.J. Brindley and R.A. Miller, TBC’s for Better Engine Efficiency,Adv. Mater. Process., Aug 1989, p 29–33

  2. W. Phucharoen, “Development of an Analytical-Experimental Method- ology for Predicting the Life and Mechanical Behavior of Thermal Bar- rier Coatings,” Ph.D. thesis, Cleveland State University, Aug 1990

  3. B.L. Ferguson, G.J. Petrus, and T.M. Krauss, “Modeling of Thermal Barrier Coatings,” NASA Contractor Report NAS3-26664, National Aeronautics and Space Administration, 12 Nov 1992

  4. J.O. Hallquist, “MAZE—An Interactive Input Generator for DYNA2D and NIKE2D,” UCID-19029, Rev. 2, Lawrence Livermore National Laboratories, 1983

  5. B. Engelmann and J.O. Hallquist, “NIKE2D, A Nonlinear, Implicit, Two-Dimensional Finite Element Code for Solid Mechanics—User Manual,” UCRL-MA-105413, Lawrence Livermore National Labora-tories, April 1991

  6. J.T. DeMasi et al., “Thermal Barrier Coating Life Prediction Model De- velopment: Phase 1 Final Report,” NASA Contract Report 182230, Na- tional Aeronautics and Space Administration, Dec 1989

  7. R.V. Hillery et al., “Thermal Barrier Coating Life Prediction Model De- velopment,” NASA Contract Report 180807, National Aeronautics and Space Administration, Nov 1988

  8. R.D. Krieg, “Numerical Integration of Some New Unified Plasticity- Creep Formulations,” SMiRT-4, M6/4,1977

  9. B.L. Ferguson, G.J. Petrus, and M. Ordillas, “A Software Tool to De- sign Thermal Barrier Coatings,” NASA Phase I Final Report, Project No. 93-1 -04.23-8477, National Aeronautics and Space Administration, 1994

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Petrus, G.J., Ferguson, B.L. A software tool to design thermal barrier coatings: a technical note. JTST 6, 29–34 (1997). https://doi.org/10.1007/BF02646309

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02646309

Navigation