Accession Number : ADA307522

Title :   Basic Properties for Comparative Evaluation of Structural Metallic Materials. Revision.

Corporate Author : AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC WASHINGTON DC

PDF Url : ADA307522

Report Date : 01 JUL 1960

Pagination or Media Count : 14

Abstract : The conditions of environment that are covered by all of the numerous aircraft and missile systems are very broad and varied The following list attempts to obtain a minimum though adequate amount cf data on a new alloy to determine whether a material is suitable for consideration in a specific design area. Such a list of properties is necessary because each new weapon system or missile will be designed to different exposure times, temperatures, deflection or creep limits, heating rates and loading rates and it will be impossible to obtain all potentially pertinent data on new alloys.

Descriptors :   *ALLOYS, GUIDED MISSILES, METALS, LOAD DISTRIBUTION, ANNEALING, MECHANICAL PROPERTIES, COMMERCE, AIRCRAFT, TENSILE PROPERTIES, THERMAL STABILITY, STRENGTH(MECHANICS), TRANSITION TEMPERATURE, HEATING, AIRFRAMES, CREEP, FATIGUE(MECHANICS), RIGIDITY, ROCKET ENGINES, CRYOGENICS, SPECIFIC HEAT, COMPRESSIVE PROPERTIES, WELDABILITY.

Subject Categories : Properties of Metals and Alloys
      Fabrication Metallurgy

Distribution Statement : APPROVED FOR PUBLIC RELEASE