2 edition of Resistance of nickel-chromium-aluminum alloys to cyclic oxidation at 1100 ̊and 1200 ̊C. found in the catalog.
Resistance of nickel-chromium-aluminum alloys to cyclic oxidation at 1100 ̊and 1200 ̊C.
Charles A. Barrett
by National Aeronautics and Space Administration, for sale by the National Technical Information Service in Washington, Springfield, Va
Written in English
|Statement||Charles A. Barrett and Carl E. Lowell ; Lewis Research Center, Cleveland, Ohio.|
|Series||NASA technical note ; NASA TN D-8255, NASA technical note -- D-8255.|
|Contributions||Lowell, Carl E., Lewis Research Center., United States. National Aeronautics and Space Administration.|
|The Physical Object|
|Pagination||, 38 p. :|
|Number of Pages||38|
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Resistance of nickel-chromium-aluminum alloys to cyclic oxidation at ̊and ̊C. Washington: National Aeronautics and Space Administration ; Springfield, Va.: For sale by the National Technical Information Service, Abstract.
A series of Co-rich alloys in the Co-Cr-Al system were cyclically oxidized in still air for 1 -hr heating cycles at ° C and 1 -hr heating cycles at °C, The specific weight-change data for each sample were then used to determine both an oxide growth constant, k 1, and a spoiling constant, k 2, for each alloy, using the regression equation ΔW/A=k 1 1/2 t 1/2 — k 2 Cited by: Oxidation and reduction of aldehydes from the standpoint of electromotive force measurements, (Lincoln, Neb., ), by Saul Bryan Arenson (page images at HathiTrust) The protection of metals from oxidation at high temperatures / (Detroit, U.S.A.: Printed for Calorizing corporation of America, c), by William Ernst Ruder and Calorizing.
RESISTANCE OF NICKEL-CHROMIUM-ALUMINUM ALLOYS TO CYCLIC OXIDATION AT 11 OOo AND 1 ° C by Charles A. Barrett and Carl E. Lowell Lewis Research Center SUMMARY Nickel- rich alloys in the nickel- chromium- aluminum (Ni- Cr- Al) system were cyclically oxidized in still air for 1-hour heating cycles at llOOo C and 1-hour.
Alloys of chromium, copper and nickel, ([Urbana, ]), by Oscar Edward Harder and David Ford McFarland (page images at HathiTrust) Preliminary study of oxide-dispersion-strengthened B prepared by mechanical alloying / (Washington, D.C.: National Aeronautics and Space Administration. Nickel Chromium Aluminum is one of numerous metal alloys sold by American Elements under the trade name AE Alloys™.Generally immediately available in most volumes, AE Alloys™ are available as bar, ingot, ribbon, wire, shot, sheet, and foil.
Ultra high purity and high purity forms also include metal powder, submicron powder and nanoscale, targets for thin film deposition, and pellets for. Nickel Chromium Aluminum Yttrium Alloy is an MCrAlY alloy with high temperature stability and corrosion resistance for MCrAlY alloy, nickel-chromium-aluminum-yttrium, Ni-Cr-Al-Y, NiCrAlY, AMPERIT Chemical Identifiers Nickel is a hard and ductile transition metal that is considered corrosion-resistant because of its slow rate of.
B Standard Specification for Nickel-Chromium-Aluminum Alloys (UNS N), Nickel-Chromium-Iron Alloys (UNS N, N, N, N, N, N, N, and N), Nickel-Chromium-Cobalt-Molybdenum Alloy (UNS N), Nickel-Iron-Chromium-Tungsten Alloy (UNS N), and Nickel-Chromium-Molybdenum-Copper Alloy (UNS N) Plate, Sheet, and Strip .