3 edition of Elevated temperature axial and torsional fatigue behavior of Haynes 188 found in the catalog.
Elevated temperature axial and torsional fatigue behavior of Haynes 188
1992 by National Aeronautics and Space Administration, US Army Aviation Systems Command, Aviation R&T Activity, For sale by the National Technical information Service in [Washington, DC], [St. Louis, Mo.], [Springfield, Va .
Written in English
|Statement||Peter J. Bonacuse and Sreeramesh Kalluri.|
|Series||NASA technical memorandum -- 105396., AVSCOM technical report -- 191-C-045., AVSCOM technical report -- 191-C-45.|
|Contributions||Kalluri, Sreeramesh., United States. Army Aviation Research and Technology Activity., United States. National Aeronautics and Space Administration.|
|The Physical Object|
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Get this from a library. Elevated temperature axial and torsional fatigue behavior of Haynes [Peter J Bonacuse; Sreeramesh Kalluri; United States. National Aeronautics and.
The results are reported for high-temperature axial and torsional low-cycle fatigue experiments performed at C in air on thin-walled tubular specimens of Haynes In-Phase and Out-of-Phase Axial-Torsional Fatigue Behavior of Haynes Superalloy at °CCited by: alloys • high temperature-high strength alloys • iron and steel alloys • cast iron alloys • wrought stainless steel • cast corrosion and heat resistant alloys* refractory metals and alloys •.
The transition from low- to high-cycle fatigue behavior occurs in the range from approximat tocycles. Many define low-cycle fatigue .