| タイトル | Evaluation of an advanced directionally solidified gamma/gamma'-alpha Mo eutectic alloy |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790012051 |
| 著者（英） | Gigliotti, M. F. X.; Henry, M. F.; Jackson, M. R.; Nelson, P. B. |
| 著者所属（英） | General Electric Co. |
| 発行日 | 1979-01-01 |
| 言語 | eng |
| 内容記述 | An attempt was made to improve on the properties of the candidate jet engine turbine blade material AG-60, a gamma/gamma prime-alpha Mo eutectic composite. Alloy 38 (AG-170) was evaluated in the greatest detail. This alloy, Ni-5.88 A1-29.74 Mo-1.65 V-1.2C Re (weight percent), represents an improvement beyond AG-60, based on mechanical testing of the transverse and/or longitudinal orientations over a range of temperatures in tension, shear, rupture, and rupture after thermal exposure. It is likely that other alloys in the study represent a similar improvement. |
| NASA分類 | METALLIC MATERIALS |
| レポートNO | 79N20222
NASA-CR-159416
SRD-78-191 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/176057 |
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