Histroy and properties of titanium; application to airframe and engine construction; commercial metal has weight of 55% of that of steel and 1 1/2 times weight of aluminum; melting point 3250 F; use of titanium for gas turbine blades; use in one of ceremals. (See also Aero Digest v 59 n 2 Aug 1949 p 38-9, 106, 108, 110)


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    Title :

    Titanium alloys for aircraft


    Additional title:

    Am Soc Naval Engrs -- J


    Contributors:


    Publication date :

    1949


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    TITANIUM ALLOYS FOR AIRCRAFT ENGINE FORGINGS

    FRAZIER, L. R. | SAE Technical Papers | 1953





    Titanium alloys and processing for high speed aircraft

    Brewer, W.D. / Bird, R.K. / Wallace, T.A. | Tema Archive | 1998