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Book Survey of Portions of the Cobalt chromium iron nickel Quaternary System

Download or read book Survey of Portions of the Cobalt chromium iron nickel Quaternary System written by E. L. Kamen and published by . This book was released on 1952 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: An isothermal survey was made of certain portions of the chromium-cobalt-nickel-iron quaternary system at 1200 degrees C. The iron content was varied up to 30 percent to include the range of commercial chromium-cobalt-nickel alloys. The component cobalt-chromium-iron ternary system was also studied.

Book Survey of Portions of the Chromium cobalt nickel molybdenum Quaternary System at 1200   C

Download or read book Survey of Portions of the Chromium cobalt nickel molybdenum Quaternary System at 1200 C written by Sheldon Paul Rideout and published by . This book was released on 1952 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: A survey was made of portions of the Chromium-cobalt-nickel-molybdenum quaternary system at 1200 degrees C by means of microscopic and x-ray diffraction studies. Since the face-centered cubic (alpha) solid solutions form the matrix of almost all practically useful high-temperature alloys, the solid solubility limits of the quaternary alpha phase were determined up to 20 percent molybdenum. The component cobalt-nickel-molybdenum, chromium-cobalt-molybdenum, and chromium-nickel-molybdenum ternary systems were also studied. The survey of these systems was confined to the determination of the boundaries of the face-centered cubic (alpha) solid solutions and of the phases coexisting with alpha at 1200 degrees C.

Book Survey of Portions of the Chromium cobalt nickel molybdenum Quaternary System at 1 200   C

Download or read book Survey of Portions of the Chromium cobalt nickel molybdenum Quaternary System at 1 200 C written by Sheldon Paul Rideout and published by . This book was released on 1953 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note   National Advisory Committee for Aeronautics

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 1262 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Note

Download or read book Technical Note written by and published by . This book was released on 1954 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of Research of the National Bureau of Standards

Download or read book Journal of Research of the National Bureau of Standards written by and published by . This book was released on 1957 with total page 868 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of Research of the National Bureau of Standards

Download or read book Journal of Research of the National Bureau of Standards written by United States. National Bureau of Standards and published by . This book was released on 1957 with total page 358 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Nickel Bulletin

Download or read book The Nickel Bulletin written by and published by . This book was released on 1951 with total page 606 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes sections "Abstracts and references" and "Patents".

Book Annual Report

    Book Details:
  • Author : United States. National Advisory Committee for Aeronautics
  • Publisher :
  • Release : 1953
  • ISBN :
  • Pages : 534 pages

Download or read book Annual Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1953 with total page 534 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report

    Book Details:
  • Author :
  • Publisher :
  • Release : 1945
  • ISBN :
  • Pages : 620 pages

Download or read book Report written by and published by . This book was released on 1945 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Report   National Advisory Committee for Aeronautics

Download or read book Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 1208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Annual Report of the National Advisory Committee for Aeronautics

Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 1200 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Book Nuclear Science Abstracts

Download or read book Nuclear Science Abstracts written by and published by . This book was released on 1975 with total page 700 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers

Download or read book Experimental Investigation of a 90 Degree Cascade Diffusing Bend with an Area Ratio of 1 45 1 and with Several Inlet Boundary Layers written by Daniel Friedman and published by . This book was released on 1952 with total page 804 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in order to determine the performance of a 90 degree cascade diffusing bend with an area ratio of 1.45:1 and a 19-inch square inlet with several inlet-boundary-layer shapes and thicknesses. The maximum mean inlet Mach number was 0.41 and the corresponding airfoil Reynolds number was 950,000. The experimental results seem to indicate that, when the duct configuration requires a bend, a certain amount of diffusion can be obtained without an appreciable rise in the total-pressure losses. If length is important, this configuration requires much less space than the usual diffuser-bend combination.