Strength of Metal Aircraft Elements ANC-5a
Washington, DC: GPO, 1949. Revised Edition. 109, wraps, 3-hole punched, illus., diagrams, references, writing on cover, covers worn and somewhat soiled. Ephemera on Detroit Stamping Co. Toggle Clamps bound in. This was issued bythe Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria of the Munitions Board Aircraft Committee. The purpose of this document was to recognize that since many aircraft manufacturers supply airplanes for both commercial and military use, standardization of the requirements of the various Government procuring or certifying agencies would be of direct benefit to the manufacturers. This publication has been prepared to eliminate the necessity for referring to different handbooks and bulletins in calculating the allowable stresses or minimum strength of typical structures. This type of technical information is increasingly scarce. It is of particular relevance to military and aviation museums, restoration facilities, military and civilian equipment collectors, and military and comercial aviation technologists. Condition: good.
Keywords: Munitions Board, Air Material, Aeronautics, Creep Rupture, Metal Fatigue, Aircraft Design, Aluminium Alloys, Magnesium Alloys
[Book #46665]
Price: $65.00