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[The Analysis of the Relationship Between Personality Traits and Changes in the Quality of Life of the Population Living in the Center of the Educational-Psychological Complex Under the Auspices of the Minister of Education of the Russian Federation].
In this article the results of the complex research of the relationship between sociocultural personality traits and changes in the quality of life of the population living in the center of the educational-psychological complex under the auspices of the Minister of Education of the Russian Federation on a group of young people aged 15-21 years are presented. The main objective of the study is to identify the population groups at a high risk of deteriorating in their quality of life. METHODS AND RESULTS. In the course of the research, and the Personality Inventory for National Research (VET2010) and the Flanders Quality of Life Scale (GLQ-15) were used. It has been found that there is a clear correlation between the personality traits and the quality of life of the population living in the center of the educational-psychological complex under the auspices of the Minister of Education of the Russian Federation on a group of young people aged 15-21 years. In particular, it has been shown that the population groups with a high neuroticism score have the biggest number of negative changes in the quality of life, compared with the population with a low score on this trait. It should be noted that different age groups of the population have different (high and low) neuroticism scores, which may contribute to a greater change in the quality of life in some age groups than in the others.Q:
How do I re-upload a NuGet package after I update the version in the.csproj file and rebuild the solution?
I am using Visual Studio 2013 Update 2 and.NET 4.5.2. I have several class library projects in my solution which I use for test automation. For most of these projects I am using NuGet for an MSTest test runner. I have updated the version in the.csproj file for some of these projects. However, the NuGet packages for the test runners are not updating. To get them to update, I delete all the.nupkg and
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Both used a similar method to find defects in aircraft and calculated risk factors.In 1935, a Boeing and Douglas company aircraft, the Douglas DC-2 was tested using the stress rupture method. In it was discovered that the aircraft was not safe for passengers, and that continued operating could cause passengers’ death.
The stress rupture method is a relatively inexpensive and non-invasive inspection technique that is mostly applied on the wings of aircraft. It differs from conventional testing methods, however, since it allows for a wide range of maximum and minimum allowable stress loads to be applied to the surface and sub-surface materials that could cause weak spots. Despite its many advantages, however, the technique has failed to gain widespread acceptance, due to its inability to be applied on a wide scale, and its inability to accurately calculate the risk of failure of the aircraft.
The stress rupture method
This method is based on the Brittle-type (Type II) failure theory. It allows for research of the strengths and failure properties of materials by causing small cracks to appear as a result of either stress increases or decreases. It is generally widely considered to be one of the least invasive and least expensive testing methods, but the results are highly inconsistent, due to the inherent differences between materials and environments. The problem stems from the fact that no single load or stress level that would cause a crack is stable over time.
In his seminal work, Dr. Robert M. Mooney applied three theoretical calculations that allowed for a more accurate measurement of the risks involved when using this testing method. These were the compressive stress. The tensile stress, and the integrated stress.
The integrated stress concept
The first is known as the Compressive Stress Index, or CRI, a calculation for computing the compressive stress level at which the material will fracture. The second is known as the Tensile Stress Index, or TSI. It is another calculation for computing the tensile stress levels at which the material will fracture. The third is known as the Integral Stress Index, or ISI, a calculation for computing the stresses in a material by adding all of the individual stresses in a material and subtracting the total compressive stresses and added tensile stress.
Table of standard compressive stress index values.
This calculation was in response to the main problem facing stress rupture testing, the problem of a fluctuating load. When dealing with stressed materials,
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