Ceramic Thermal Barrrier Coatings for Cooled Turbines-Reference-Cited by-同舟云学术

Ceramic Thermal Barrrier Coatings for Cooled Turbines

Published:1977-05 Issue:5 Volume:14 Page:487-493
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Liebert Curt H.¹,Stepka Francis S.¹

Affiliation:

1. NASA Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.58805

Reference15 articles.

1. K MAR-M-302 Metal wall 4.9xlO"3T + 18.0 300 - 1260 6

2. (research engine) MAR-M-509 Metal wall (advan- S.OxlO"2T + 3.7 590 - 1370 10

3. Price, H.G.,Schacht, R.L., and Quentmeyer, R.J. "Reliability and Effective Thermal Conductivity of Three Metallic-Ceramic Composite Insulating Coatings on Cooled Hydrogen-Oxygen Rockets,'' NASA TN D-7392, Nov. 1973.

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