Effect of Correlations on the Equation of State of an Electron Gas (open access)

Effect of Correlations on the Equation of State of an Electron Gas

An attempt to apply quantitatively the equation of state of a free electron gas to relatively low temperatures in order to emphasize correlation effects.
Date: January 14, 1955
Creator: Ferrell, Richard
System: The UNT Digital Library
Detection of Airborne Beryllium Dust : Monthly Report Covering the Period from May1 to June 1, 1955 (open access)

Detection of Airborne Beryllium Dust : Monthly Report Covering the Period from May1 to June 1, 1955

During this period a prototype gamma ray detection system was assembled and data was obtained on samples of beryllium salts on filter paper under a variety of conditions. Ordinarily either a scaler-register combination or the CRM-recorder combination would be sufficient for obtaining data. Both units have been used here in order to utilize the particular advantages of each system. The scaler-register unit was employed for obtaining precise data over short intervals while the CRM-recorder was used to maintain a check on stability over longer intervals of time.
Date: June 14, 1955
Creator: McCarty, R. G.
System: The UNT Digital Library
Turbine Start-Up. Section I. Second Performance. Core I, Seed 1. Test Results DL-S-179 (open access)

Turbine Start-Up. Section I. Second Performance. Core I, Seed 1. Test Results DL-S-179

The purpose of the test was to insure satisfactory operation of the turbine after overhaul of the turbine which was completed February 1, 1959. The operation of the turbine during this start-up was satisfactory.
Date: December 14, 1959
Creator: unknown
System: The UNT Digital Library
Low Speed Wind Tunnel Tests of Several Airfoil Sections Through 360 ° Angle of Attack (open access)

Low Speed Wind Tunnel Tests of Several Airfoil Sections Through 360 ° Angle of Attack

A series of two-dimensional airfoils were run through a complete 360 ° angle of attack range to determine their low-speed force characteristics. The airfoils were chosen in an attempt to vary as many parameters (such as thickness, camber, thickness distribution, etc.) as possible with the limited number of shapes that time permitted. All airfoils tested had lift curves with two distinct stalls and quite similar drag curves between 0 ° and 90 ° angle of attack. The highly cambered sections developed peculiar characteristics in the inverted and trailing edge forward positions, as might be expected. The effective test Reynolds number of 0.81 x 10(6) based on the model chord of one foot.
Date: October 14, 1954
Creator: Reed, James F.
System: The UNT Digital Library