Author: J. M. AllenPublisher:
ISBN:
Category : Metals
Languages : en
Pages : 52
Book Description
Environmental Factors Influencing Metals Applications in Space Vehicles
Author: J. M. AllenDesign Considerations in Selecting Materials for Large Solid-propellant Rocket-motor Cases
Author: Charles Wesley BertPublisher:
ISBN:
Category : Heat resistant alloys
Languages : en
Pages : 80
Book Description
Review of Current Data on the Tensile Properties of Metals at Very Low Temperatures
Author: James Edward CampbellPublisher:
ISBN:
Category : Liquid hydrogen
Languages : en
Pages : 90
Book Description
Gas-pressure Bonding
Author: S. J. PaprockiPublisher:
ISBN:
Category : Diffusion bonding (Metals)
Languages : en
Pages : 56
Book Description
Stress-corrosion Cracking of High-strength Stainless Steels in Atmospheric Environments
Author: C. J. SlunderPublisher:
ISBN:
Category : Corrosion and anti-corrosives
Languages : en
Pages : 44
Book Description
Oxidation of Tungsten
Author: Vincent David BarthPublisher:
ISBN:
Category : Tungsten
Languages : en
Pages : 192
Book Description
The report presents a detailed review of available information on the oxidation of W and its alloys. W is relatively inert below 700 C. As the temperature is increased above this level, however, oxidation becomes progressively more rapid, reaching catastrophic rates at temperatures around 1200 C and above. Various theories for the mechanism and rates of W oxidation at different temperatures are reviewed, and the effect of pressure and water vapor on the stability of W oxides is discussed in detail. The elevatedtemperature reactions of W with other materials, such as refractory oxides, and with gases other than oxygen also are covered. Information on the protection of W by alloying and coating is included. (Author).
Statistical Analysis of Tensile Properties of Heat-treated Ti-4A1-3Mo-1V and Ti-2.5A1-16V Sheet
Author: G. H BeattyPublisher:
ISBN:
Category : Metals
Languages : en
Pages : 54
Book Description
IN THE SOLUTION TREATED AND AGED CONDITION, Ti4Al-3Mo-1V has a higher ultimate strength than does Ti-2.5Al-16V, but the two alloys are about even in yield strength and elongation. In the solution-treated condition, Ti-4Al-3Mo-1V is unquestionably stronger than Ti-2.5Al-16V. These conclusions are independent of producer. There is not much difference in the same alloy produced by different companies. The alloys developed under the Titanium-Alloy Sheet-Rolling Program would not endure the most critical interpretation of release property specifications. On the other hand, these alloys come reasonably close to specifications. A complete set of release property specifications is available only for specimens that have been solution treated and aged. Such specimens do not all exhibit the desired ultimate and yield strength, but the percentage of rejects is small enough to be encouraging. (Author).
Design Information on AM-350 Stainless Steel for Aircraft and Missiles
Author: R. J. FavorPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 58
Book Description
The Factors Influencing the Fracture Characteristics of High-strength Steel
Author: Charles W. MarschallPublisher:
ISBN:
Category : Steel, High strength
Languages : en
Pages : 46
Book Description
Physical Metallurgy of Nickel-base Superalloys
Author: C. H. LundPublisher:
ISBN:
Category : Heat resistant alloys
Languages : en
Pages : 54
Book Description