Download Free Tensile Properties Of Inconel And Rs 120 Titanium Alloy Sheet Under Rapid Heating And Constant Temperature Conditions Book in PDF and EPUB Free Download. You can read online Tensile Properties Of Inconel And Rs 120 Titanium Alloy Sheet Under Rapid Heating And Constant Temperature Conditions and write the review.

Results are presented of some rapid-heating tests of some sheet materials - 7075-T6 and 2024-T3 (formerly 75S-T6 and 24S-T3, respectively) aluminum alloys, Inconel, and RS-120 titanium alloy - which are part of an investigation of a number of structural materials. The materials were tested at temperature rates from 0.2 degree F to 100 degrees F per second under constant-load conditions.
The linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the theory to large attenuations; and (c) transition effects are considered. Curves are presented for predicting attenuation for shock pressure ratios up to 20 and a range of shock-tube Reynolds numbers. Comparison of theory and experimental data for shock wave strengths between 1.5 and 10 over a wide range of Reynolds numbers shows good agreement with the nonlinear theory evaluated for a transition Reynolds nuniber of 2.5 million.