Application of single crystal superalloys for earth-to-orbit propulsion systems
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
2. NASA, Marshall Space Flight Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1976
Reference14 articles.
1. Rocket Enaine Turbooumo Turbine Blades." , Aovancc&h Press,rc -%rea and S.T. h., eds.asninqron, 7.C. 1985, pp.110-131.
2. Gry'and Materials on Low Cycle Fatigue Life of Turbine Blades i n LOX/Hydrogen Rocket Engines," AIAA Paper 86-1443, June 1986. 4. Gabb, T.P., Gayda, J. and Miner, R.V.
3. Processing Conditions and Heat Treatments on the Mechanical Properties of a Single Crystal Superalloy," ONERA-TP-1985-15, Feb. 1985. 6. Jablonski, D.A. and Sargent, S. "Anisotropic
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1. The effect of porosity and γ-γ′ eutectic content on the fatigue behavior of hydrogen charged PWA 1480;Scripta Metallurgica et Materialia;1991-11
2. Solutal partition coefficients in nickel-based superalloy PWA-1480;Materials Science and Engineering: A;1991-07
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