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Aerothermodynamics of Gas Turbine and Rocket Propulsion, Volume 1
Gordon C. Oates
Limited preview - 1997
0.300-inch-diameter round polished 1-inch-diameter ADDITIONAL FATIbUE TEere addNion Aluminum Company oI aluminum-alloy Appreciable Trans band of results cast test bars CommNtee ior Aeronautics Company oI America cored hole type cycles to failure degree of porosity design details direct-stress fatigue specimens direct-stress fatigue test dmmeter EFFECTe OF DEeIDE ends of type fatigue test results FRTM Heavy Long hole type IB hole was reamed I. D. Eaton irom the butt machined from butt Matermls Minimum stress NACA RM NACA Technical Note National Advisory CommNtee numbers of cycles o o o oi earaer tests open hole osshington oven in NACA plate-type speci plate-type specimens wNh porosity ratings rally rally rally reamed hole round polished specimens round specimens sand-cast specimens sarcimens separately cast test Slight Long Slight Trans specimen types SPECIMENS MACHINED specimens wNh varmtions static and iatiaue stress concentration factors stress iatiaue tests stress ratio Tensile test section Ydera