ASD Technical Report, Numéro 61,Partie 529Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962 |
Table des matières
INTRODUCTION | 1 |
SCOPE OF INVESTIGATION | 3 |
SPECIMEN PREPARATION | 7 |
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Expressions et termes fréquents
1600 Temperature 355 Exposed Average Based on Original Bearing Yield Strength Cent Fory Cent Ftu Cold Reduced Compressive Modulus COMPRESSIVE TANGENT MODULUS Compressive Yield Strength Effect of Temperature Exposed 0.5 Hours Exposed 100 Hours EXPOSURE TIMES Cont'd F EFFECT F FIGURE Fory at Room Ftu at Room HOURS Per Cent Modulus of Elasticity Notched Strength Ratio Notched Ultimate Tensile Number Test Temperature OHIO STATE UNIVERSITY ORIGINAL AND FINAL Ph15-7Mo Exposed René 41 Exposed Room Temperature 100 Specimen Number Test Stainless Steel Exposed Steel Exposed 0.5 Steel Exposed 100 Strength hr Strength of 301 STRENGTH OF N-155 Strength of Ph15-7Mo Strength of René TANGENT MODULUS CURVES TEMPERATURE ON BEARING TEMPERATURE ON COMPRESSIVE TEMPERATURE ON ELONGATION TEMPERATURE ON MODULUS Temperature on Notched TEMPERATURE ON RUPTURE Temperature on Tensile TEMPERATURE ON ULTIMATE TEMPERATURES AND EXPOSURE TENSILE PROPERTIES Tensile Stress-Strain Curves Tensile Yield Strength Ultimate Bearing Strength Ultimate Tensile Strength UNIVERSITY LIBRARIES VARIOUS TEMPERATURES