EFFECTS OF VARIOUS AGING HEAT TREATMENTS AND SOLUTION-ANNEALING AND AGING HEAT TREATMENTS ON TENSILE, CREEP, AND STRESS-RUPTURE STRENGTHS OF INCONEL X SHEET TO TEMPERATURES OF 1,400 F
Technical Report
·
OSTI ID:4128906
The effects of six different heat treatments are presented on the tensile strength, on the minimum creep rate, on the 0.2% creep strength in 5 and 10 hr, and on the 10and 100-hr stress-rupture strength of Inconel X sheet at greatest tensile strength for all test temperatures. Aging treatments, in general, were superior for the 0.2% creep strength in 5 and 10 hr and the 10-hr stress-rupture strength at 1,000, l,200, and l,400 deg F. The solutionannealing and aging treatments had the best 100-hr stressrupture strength at 1,200 deg F, whereas a short aging treatment was superior at 1,400 deg F. (auth)
- Research Organization:
- National Aeronautics and Space Administration. Langley Research Center, Langley Field, Va.
- NSA Number:
- NSA-15-006381
- OSTI ID:
- 4128906
- Report Number(s):
- NASA-TN-D-374
- Country of Publication:
- United States
- Language:
- English
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