Accession Number : ADA322636
Title : Metallic Materials and Elements for Aerospace Vehicle Structures. Military Handbook. Volume 2.
Corporate Author : WRIGHT LAB WRIGHT-PATTERSON AFB OH MATERIALS DIRECTORATE
PDF Url : ADA322636
Report Date : 01 NOV 1994
Pagination or Media Count : 776
Abstract : This book contains the engineering properties and related characteristics of metallic materials used in aircraft and missile structural applications. Titanium is a relatively lightweight, corrosion-resistant structural material that can be strengthened greatly through alloying and, in some of its alloys, by heat treatment. Among its advantages for specific applications are: good strength to weight ratio, low density, low coefficient of thermal expansion, good corrosion resistance, good oxidation resistance at intermediate temperatures, good toughness, and low heat treating temperature during hardening, and others.
Descriptors : *MECHANICAL PROPERTIES, *PHYSICAL PROPERTIES, *AEROSPACE CRAFT, *TITANIUM ALLOYS, STRESS STRAIN RELATIONS, GUIDED MISSILES, AIRCRAFT, STRUCTURAL PROPERTIES, TOUGHNESS, RUPTURE, HEAT TREATMENT, CRACK PROPAGATION, CORROSION RESISTANCE, COEFFICIENTS, THERMAL EXPANSION, CREEP, TITANIUM, LOW DENSITY, OXIDATION RESISTANCE, HANDBOOKS, STRENGTH WEIGHT RATIO, HARDENING.
Subject Categories : Research and Experimental Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE