Frequency Components of a Step Function and a Sinusoid (open access)

Frequency Components of a Step Function and a Sinusoid

Fourier analyses are made on two functions. The first is a step function forward from periodic samples of a sinusoid. If the frequency of the sinusoid is less than one-half of the sampling frequency, it is shown that the step function has no frequency components less than one-half of the sampling frequency other than that of phase, and duration with respect to the interval of the analysis. It is shown that the insertion of a blank space in the period of analysis reduces greatly the uncertainty of the amplitude of the initial sinusoid as estimated from the results of the Fourier analysis. The results of the analyses are useful in the design and evaluation of certain analog data-analyzing systems.
Date: May 10, 1955
Creator: McGehee, R. M.
System: The UNT Digital Library
Mechanical and Physical Properties of Uranium: Chapter 8 of Nuclear Metallurgy Lectures (open access)

Mechanical and Physical Properties of Uranium: Chapter 8 of Nuclear Metallurgy Lectures

A knowledge of the mechanical and physical properties of uranium is important in understanding and explaining its pile behavior. The effects of irradiation on the properties of uranium will be dealt with in another chapter. However, it is important to know and understand the pre-irradiation properties of uranium prior to investigating the effects of irradiation.
Date: May 10, 1955
Creator: Rueschen, R. E.
System: The UNT Digital Library
Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams (open access)

Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams

Report presenting some experimental and theoretical studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams as a way to investigate problems associated with propulsive jets. A variety of variables for each case are considered, including jet Mach number, nozzle divergence angle, jet static-pressure ratio, free-stream Mach number, and specific heat ratios.
Date: May 10, 1955
Creator: Love, Eugene S. & Grigsby, Carl E.
System: The UNT Digital Library