Design Information on Nickel-base Alloys for Aircraft and Missiles
Author : R. J. Favor
Publisher :
Page : 168 pages
File Size : 21,37 MB
Release : 1960
Category : Airplanes
ISBN :
Author : R. J. Favor
Publisher :
Page : 168 pages
File Size : 21,37 MB
Release : 1960
Category : Airplanes
ISBN :
Author : W. P. Achbach
Publisher :
Page : 90 pages
File Size : 20,76 MB
Release : 1961
Category : Airplanes
ISBN :
Author : R. M. Evans
Publisher :
Page : 86 pages
File Size : 29,77 MB
Release : 1962
Category : Brazing alloys
ISBN :
Author : R. J. Favor
Publisher :
Page : 52 pages
File Size : 22,15 MB
Release : 1960
Category : Airplanes
ISBN :
Author : R. J. Favor
Publisher :
Page : 68 pages
File Size : 17,35 MB
Release : 1960
Category : Airplanes
ISBN :
Author : R. J. Favor
Publisher :
Page : 58 pages
File Size : 43,66 MB
Release : 1961
Category : Airplanes
ISBN :
Author : C. H. Lund
Publisher :
Page : 54 pages
File Size : 10,20 MB
Release : 1961
Category : Heat resistant alloys
ISBN :
Author : M. E. Landstone
Publisher :
Page : 162 pages
File Size : 24,94 MB
Release : 1960
Category : Nickel alloys
ISBN :
Author : R. J. Favor
Publisher :
Page : 50 pages
File Size : 45,79 MB
Release : 1960
Category : Airplanes
ISBN :
Author : Albert G. Imgram
Publisher :
Page : 80 pages
File Size : 44,15 MB
Release : 1963
Category : Heat resistant alloys
ISBN :
This report summarizes the present knowledge concerning the relationship among fabrication history, metallurgical structure, and the mechanical properites of the refractory metals columbium, tantalum, bolybdenum, and tungsten, and their alloys. These are the refractory metals currently reveiveing the most attention for aerospace applications, and are therefore the materials considered in this survey. The report is organized into three main sections, titled ''Fabrication'', ''Microstructure and Alloying'', and ''Interstitial Impurities''. The data presented were selected as those which best illustrate the topics discussed. Descriptions of the metaljurgical principles involved are included. Suggestions for optimizing mechanical properties by controlling metallurgical structure are made where possible. (Author).