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1

Ellis, David L. Hot corrosion of the B2 nickel aluminides. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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2

Guha, Sumit. Improving the low temperature ductility of NiAl. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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3

Ansari, Iqbal. Irradiation-Induced Creep and Microstructural Development in Precipitation-Hardened Nickel-Aluminum Alloys. Julich, W. Ger: Zentralbibliothek der Kernforschungsanlage, 1985.

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4

Dunning, J. S. Effect of aluminum additives on sulfidation resistance of some Fe-Cr-Ni alloys. Washington, DC: Dept. of the Interior, 1989.

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5

Dunning, J. S. Effects of Al additions on sulfidation resistance of some Fe-Cr-Ni alloys. Washington, D.C: Bureau of Mines, U.S. Dept. of the Interior, 1989.

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6

C, Deevi Seetharama, ASM International. Materials Science Critical Technologies., and ASM International. Specialty Materials Critical Technologies Sector., eds. International Symposium on Nickel and Iron Aluminides: Processing, Properties, and Applications: Proceedings from Materials Week '96, 7-9 October 1996, Cincinnati Convention Center, Cincinnati, Ohio. Materials Park, OH: ASM International, 1997.

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7

de, Villiers H. L., ed. The physics of creep: Creep and creep-resistant alloys. London: Taylor & Francis, 1995.

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8

Kozubski, Rafał. "Order-order" reactions in Ni₃Al-based intermetallic compounds with L1₂-type superstructure. Kraków: Wyd. Uniwersytetu Jagiellońskiego, 1996.

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9

Whittenberger, J. Daniel. Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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10

United States. National Aeronautics and Space Administration., ed. The influence of chromium on structure and mechanical properties of B2 nickel aluminide alloys. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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11

United States. National Aeronautics and Space Administration., ed. The influence of chromium on structure and mechanical properties of B2 nickel aluminide alloys. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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12

Physical and mechanical metallurgy of NiAl. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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13

R, Bowman R., Nathal Michael V, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Physical and mechanical metallurgy of NiAl. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

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14

Patchett, Joseph Allan. The kinetics of the peritectic reactions in aluminum-nickel alloys. 1988.

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15

Manabu, Ueno, Noguchi Osamu, and United States. National Aeronautics and Space Administration., eds. Martensitic transformations and microstructures in sintered NiAl alloys. Washington, DC: National Aeronautics and Space Administration, 1988.

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16

Osamu, Noguchi, Ueno Manabu, and United States. National Aeronautics and Space Administration., eds. Martensitic transformation and microstructures in sintered NiAl alloys. Washington, D.C: National Aeronautics and Space Administration, 1988.

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17

Manifestations of dynamic strain aging in soft-oriented NiAl single crystals. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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18

Deformation mechanisms of NiAl cyclicly deformed near the brittle-to-ductile transition temperature. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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19

J, Kaufman M., and Noebe R. D, eds. Manifestations of dynamic strain aging in soft-oriented NiAl single crystals. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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20

United States. National Aeronautics and Space Administration., ed. Electron diffraction evidence for the ordering of excess nickel atoms by relation to stoichiometry in nickel-rich B'-NiAl formation of a nickel-aluminum (Ni2Al) superlattice. Washington, DC: National Aeronautics and Space Administration, 1988.

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21

R, Bowman R., Nathal Michael V, and United States. National Aeronautics and Space Administration., eds. Review of the physical and mechanical properties and potential applications of the B2 compound NiAl. [Washington, DC: National Aeronautics and Space Administration, 1992.

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22

J, Cawley, Greenwood G. W, Strang A, and Institute of Materials (London, England)., eds. Microstructural stability of creep resistant alloys for high temperature plant applications. London: IOM Communications, 1998.

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23

D, Noebe R., Darolia R, and United States. National Aeronautics and Space Administration., eds. Crystallography of the NiHfSi phase in a NiAl (0.5 Hf) single-crystal alloy. [Washington, DC: National Aeronautics and Space Administration, 1996.

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24

(Editor), Andrew Strang, J. Cawley (Editor), and G. W. Greenwood (Editor), eds. Microstructural Stability of Creep Resistant Alloys for High Temperature Plant Applications (Microstructure of High Temperature Materials). Ashgate Publishing, 1998.

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25

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Effects of chromium and aluminum on mechanical and oxidation properties of iron-nickel-base superalloys based on CG-27. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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26

Thermodynamic analysis of compatibility of several reinforcement materials with beta phase NiAl alloys. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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27

Strain aging behavior in NiAl microalloyed with interstitial and substitutional solutes. [Washington, DC: National Aeronautics and Space Administration, 1997.

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28

Observations of dynamic strain aging in polycrystalline NiAl. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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29

L, Weaver M., and United States. National Aeronautics and Space Administration., eds. Observations of static strain-aging in polycrystalline NiAl. [Washington, DC: National Aeronautics and Space Administration, 1996.

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30

D, Noebe R., and Kaufman M. J, eds. Observations of dynamic strain aging in polycrystalline NiAl. [Washington, D.C: National Aeronautics and Space Administration, 1997.

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31

L, Regelʹ L., Smith Reginald W, and United States. National Aeronautics and Space Administration., eds. Use of microgravity to control the microstructure of eutectics: NASA grant NAG8-1266; progress report, 1 March 1998. [Washington, DC: National Aeronautics and Space Administration, 1998.

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32

R, Browning, and Lewis Research Center, eds. Current viewpoints on oxide adherence mechanisms. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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33

Composition dependence of the M, temperature in the Ý'NiAl compound. Washington, DC: National Aeronautics and Space Administration, 1988.

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34

R, Johnson D., and United States. National Aeronautics and Space Administration., eds. NiAl-based polyphase in situ composites in the NiAl-Ta-X (X = Cr, Mo, or V) systems. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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35

High temperature composites. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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36

Microstructure and properties of cryomilled nickel aluminide extruded with chromium or molybdenum. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

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37

D, Noebe R., Kaufman M. J, and United States. National Aeronautics and Space Administration., eds. The influence of C and Si on the flow behavior of NiAl single crystals. [Washington, DC: National Aeronautics and Space Administration, 1996.

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