Location

La Jolla, CA

Start Date

1-1-1993 12:00 AM

Description

For advanced aircraft gas-turbine engines greater efficiencies and higher thrust are demanded. One possibility to achieve this is to increase the gas temperature at the turbine-section. Then thermal barrier coatings are necessary to protect the metallic structures.

Book Title

Review of Progress in Quantitative Nondestructive Evaluation

Volume

12B

Chapter

Chapter 6: Material Properties

Section

Thin Films and Coatings

Pages

1915-1921

DOI

10.1007/978-1-4615-2848-7_245

Language

en

File Format

application/pdf

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Jan 1st, 12:00 AM

Ultrasonic Attenuation of Water-Infiltrated Thermal Barrier Coatings

La Jolla, CA

For advanced aircraft gas-turbine engines greater efficiencies and higher thrust are demanded. One possibility to achieve this is to increase the gas temperature at the turbine-section. Then thermal barrier coatings are necessary to protect the metallic structures.