Theoretical-Experimental Model for Predicting Crack Growth Rate in Structural Alloys of Aircraft Gas Turbine Engine Disks with Regard to Fatigue and Creep

✍ Scribed by V. V. Pokrovskii; V. N. Ezhov; V. G. Sidyachenko

• Publisher: Springer
• Year: 2005
• Tongue: English
• Weight: 144 KB
• Volume: 37
• Category: Article
• ISSN: 0039-2316
• DOI: 10.1007/s11223-006-0002-0