Thermal and Oxidation Response of UHTC Leading Edge Samples Exposed to Simulated Hypersonic Flight Conditions-Reference-Cited by-同舟云学术

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Thermal and Oxidation Response of UHTC Leading Edge Samples Exposed to Simulated Hypersonic Flight Conditions

Published:2013-02-12 Issue:3 Volume:96 Page:907-915
ISSN:0002-7820
Container-title:Journal of the American Ceramic Society
language:en
Short-container-title:J. Am. Ceram. Soc.

Author:

Parthasarathy Triplicane A.¹²,Petry Melvin D.¹²,Cinibulk Michael K¹,Mathur Tarun³,Gruber Mark R.⁴

Affiliation:

1. Air Force Research Laboratory; Materials and Manufacturing Directorate; Wright-Patterson AFB; 45433-7817 Ohio

2. UES, Inc.; Dayton 45432 Ohio

3. ISSI; Dayton Ohio

4. Air Force Research Laboratory; Aerospace Systems Directorate; Wright-Patterson AFB; Ohio

Funder

USAF

US Air Force Office of Scientific Research

Publisher

Wiley

Subject

Materials Chemistry,Ceramics and Composites

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/jace.12180/fullpdf

Reference39 articles.

1. Ames Research Staff Equations, Tables and Charts for Compressible Flow 1953

2. On the Boundary Layer Equations in Hypersonic Flow and Their Approximate Solutions;Lees;J. Aero. Sci.,1953

3. Theory of Stagnation Point Heat Transfer in Dissociated Air;Fay;J. Aero. Sci.,1958

4. Oxidation-Based Materials Selection for 2000°C+ Hypersonic Aerosurfaces: Theoretical Considerations and Historical Experience;Opeka;J. Mater. Sci.,2004

5. Designing for Ultrahigh-Temperature Applications: The Mechanical and Thermal Properties of HfB2, HfCx, HfNx and a-Hf(N);Wuchina;J. Mater. Sci.,2004

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