Grain Refinement of Uranium by Alloying (open access)

Grain Refinement of Uranium by Alloying

Binary alloys of uranium with 38 elements in the range 0.01 to 1.0 at.% were made. Three alloys having nominal compositions of 0.01, 0.1, and 1.0 at.% were made with most of the elements, and in addition, 12 ternary and quaternary alloys were made. The alloys were cast, rolled to 7/8-inch-diameter bars, heat treated, and examined for grain size.
Date: June 1, 1951
Creator: Saller, Henry A.; Keeler, J. R. & Eddy, N. S.
Object Type: Report
System: The UNT Digital Library
Jacketing of Uranium for High-Temperture Service (open access)

Jacketing of Uranium for High-Temperture Service

From introduction: "The work covered in this report is a portion of the experimental research undertaken for the design of a uranium-containing metallic fuel rod for operation in air at 1090 C...This report deals with that phase which involved the testing and evaluation of various metals as barrier costs between uranium alloys, and low-carbon steel. The work is of a preliminary nature and is concerned more with a comparison of the various barrier metals than with the acquisition of numerical data, e.g., diffusion coefficients."
Date: June 1, 1951
Creator: Saller, Henry A. & Stacy, J. T.
Object Type: Report
System: The UNT Digital Library
Radiation Safety and Control Training Manual (open access)

Radiation Safety and Control Training Manual

Introduction: The Laboratory follows the recommendations of the National Committee on Radiation Protection concerning permissible exposure limits for those working with radiation. A system of controls and regulations has been established which should ensure that no person at the Laboratory will receive more than the permissible exposure. This manual is intended to provide the minimum background necessary for intelligent cooperation with the regulations.
Date: June 1, 1961
Creator: Oak Ridge National Laboratory
Object Type: Report
System: The UNT Digital Library
Engineering Evaluation of a Mixed Alloy Fuel Element Irradiated at Elevated Temperatures in the SRE (open access)

Engineering Evaluation of a Mixed Alloy Fuel Element Irradiated at Elevated Temperatures in the SRE

Abstract: A fuel material evaluation was made by destructively examining a full-scale experimental fuel element, irradiated in the SRE to a maximum of 850 Mwd/MTU.
Date: June 1, 1960
Creator: Ballif, J. L.; Hayward, B. R. & Walter, J. W.
Object Type: Report
System: The UNT Digital Library
The Contamination of Cooling Water by a P-9 Plant (open access)

The Contamination of Cooling Water by a P-9 Plant

The following sources of contamination in cooling water of the P-9 plant are considered: (1) Fission recoils, (2) Corrosion of metal, (3) Recoil from aluminum, (4) Induced activity in the water. It is found that for a P-9 plant of 3.5 x 10(4) KW contamination of the river at "X" should not exceed the .1 r criterion unless coating failure occurs. Tables of the amount of coating failure permissible are given as a function of holdup time.
Date: June 1, 1943
Creator: Friedman, Francis L. (Francis Lee), 1918-
Object Type: Report
System: The UNT Digital Library
Representation of Slowing Down Functions in Water by Synthetic Kernels (open access)

Representation of Slowing Down Functions in Water by Synthetic Kernels

Fermi, Anderson, and Nagle's experimental distribution of Indium resonance neutrons around a point source of fission neutrons in water has been fitted by analytic expressions which are source functions in the two-group, three-group, Fermi and Christy-Wheeler pile theory. The Christy-Wheeler function (exponential followed by a Gaussian) is the best fit; the two-group function (exponential) is slightly better than the Fermi Gaussian.
Date: June 1, 1944
Creator: Cahn, Albert, Jr.
Object Type: Report
System: The UNT Digital Library
Liquid Metal Loops Irradiated on the ORNL Graphite Reactor and the LITR (open access)

Liquid Metal Loops Irradiated on the ORNL Graphite Reactor and the LITR

From abstract: Liquid alkali metals were circulated in a series of structural alloy loops under reactor radiation at high temperature. The first of these loops was a lithium-stainless steel (type 316) system, and the remainder were sodium-Inconel. No effect of radiation other than radioactivation was found. Mass transfer and metallurgical processes attributable to the operating temperatures were observed."
Date: June 1, 1959
Creator: Parkinson, W. W. & Sisman, O.
Object Type: Report
System: The UNT Digital Library
A Comparison of the Maneuvering Performance of a Monowing Versus a Cruciform Missile (open access)

A Comparison of the Maneuvering Performance of a Monowing Versus a Cruciform Missile

Memorandum presenting an assessment of the importance of the addition lag of the monowing versus a cruciform shape on a missile.
Date: June 1, 1955
Creator: Matthews, Howard F. & Schmidt, Stanley F.
Object Type: Report
System: The UNT Digital Library
Large-scale flight measurements of zero-lift drag at Mach numbers form 0.86 to 1.5 of a wing-body combination having a 60 degree triangular wing with NACA 65A003 sections (open access)

Large-scale flight measurements of zero-lift drag at Mach numbers form 0.86 to 1.5 of a wing-body combination having a 60 degree triangular wing with NACA 65A003 sections

Report presenting flight testing at high-subsonic and supersonic speeds at high Reynolds numbers to determine the zero-lift drag of a fin-stabilized body and a wing-body combination. The body was parabolic in profile, had a fineness ratio of 10, and a ratio of body frontal area to wing area to 0.306.
Date: June 1, 1950
Creator: Nelson, Robert L.
Object Type: Report
System: The UNT Digital Library
Low-Speed Investigation of Deflectable Wing-Tip Elevators on a Low-Aspect-Ratio Untapered 45 Degree Sweptback Semispan Wing With and Without an End Plate (open access)

Low-Speed Investigation of Deflectable Wing-Tip Elevators on a Low-Aspect-Ratio Untapered 45 Degree Sweptback Semispan Wing With and Without an End Plate

Report presenting an investigation to determine the longitudinal control characteristics of deflectable wing-tip elevators on a low-aspect-ratio, untapered, 45 degree sweptback semispan wing. The elevators had triangular and parallelogrammic plan forms and flat-plate profiles. Results include the elevator effectiveness and comparison of the elevator effectiveness of deflectable wing-tip controls and trailing-edge flap-type controls.
Date: June 1, 1950
Creator: Fischel, Jack & O'Hare, William M.
Object Type: Report
System: The UNT Digital Library
Equations for the Design of Two-Dimensional Supersonic Nozzles (open access)

Equations for the Design of Two-Dimensional Supersonic Nozzles

"Equations are presented for obtaining the wall coordinates of two-dimensional supersonic nozzles. The equations are based on the application of the method of characteristics to irrotational flow of perfect gases in channels. Curves and tables are included for obtaining the parameters required by the equations for the wall coordinates. A brief discussion of characteristics as applied to nozzle design is given to assist in understanding and using the nozzle-design method of this report. A sample design is shown" (p. 1).
Date: June 1, 1948
Creator: Pinkel, I. Irving
Object Type: Report
System: The UNT Digital Library
A Thermodynamic Study of the Turbojet Engine (open access)

A Thermodynamic Study of the Turbojet Engine

"Charts are presented for computing thrust, fuel consumption, and other performance values of a turbojet engine for any given set of operating conditions and component efficiencies. The effects of pressure losses in the inlet duct and the combustion chamber, of variation in physical properties of the gas as it passes through the system, of reheating of the gas due to turbine losses, and of change in mass flow by the addition of fuel are included. The principle performance chart shows the effects of primary variables and correction charts provide the effects of secondary variables and of turbine-loss reheat on the performance of the system" (p. 599).
Date: June 1, 1946
Creator: Pinkel, Benjamin & Karp, Irving M.
Object Type: Report
System: The UNT Digital Library
Direct Measurements of Skin Friction (open access)

Direct Measurements of Skin Friction

"A device has been developed to measure local skin friction on a flat plate by measuring the force exerted upon a very small movable part of the surface of the flat plate. These forces, which range from about 1 milligram to about 100 milligrams, are measured by means of a reactance device. The apparatus was first applied to measurements in the low-speed range, both for laminar and turbulent boundary layers. The device was then applied to high-speed subsonic flow and the turbulent-skin-friction coefficients were determined up to a Mach number of about 0.8" (p. 281).
Date: June 1, 1951
Creator: Dhawan, Satish
Object Type: Report
System: The UNT Digital Library
Investigation of Separation of the Turbulent Boundary Layer (open access)

Investigation of Separation of the Turbulent Boundary Layer

"An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gradients sufficient to cause flow separation. The Reynolds number was high, but the speeds were entirely within the incompressible flow range. The investigation consisted of measurements of mean flow, three components of turbulence intensity, turbulent shearing stress, and correlations between two fluctuation components at a point and between the same component of different points" (p. 1).
Date: June 1, 1949
Creator: Schubauer, G. B. & Klebanoff, P. S.
Object Type: Report
System: The UNT Digital Library
Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection (open access)

Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection

From Summary: "Curves are presented that show the theoretical performance of the augmentation method for various amounts of water injected and the effects of varying flight Mach number, altitude, ambient-air temperature, ambient relative humidity, compressor pressure ratio, and inlet-diffuser efficiency. Numerical examples, illustrating the use of the psychrometric chart and the Mollier diagram in calculating both compressor-inlet and compressor-outlet conditions when water is injected at the compressor inlet, are presented."
Date: June 1, 1950
Creator: Wilcox, E. Clinton & Trout, Arthur M.
Object Type: Report
System: The UNT Digital Library
Analytical evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 (open access)

Analytical evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1

From Summary: "The effects of variation in inlet-air temperature, combustion pressure, and boron or pentaborane concentration on combustion performance were discussed. It was shown how the theoretical data herein could be employed in obtaining the combustion efficiency of experimental combustors. Data were presented by which combustion efficiencies obtained with a water-quench heat balance could be adjusted for the heat of dissociation of the combustion products."
Date: June 1, 1955
Creator: Tower, Leonard K.
Object Type: Report
System: The UNT Digital Library
Experimental Evaluation of Boron-Hydrocarbon Slurry in a 16-Inch Ram-Jet Combustor (open access)

Experimental Evaluation of Boron-Hydrocarbon Slurry in a 16-Inch Ram-Jet Combustor

"The combustion efficiency of a 50-percent-boron-hydrocarbon slurry was evaluated in a 16-inch ram-jet burner. A peak slurry combustion efficiency of 75 percent was usually obtained, and a value of 84 percent was once measured. The connected-pipe burner was run at a simulated flight condition of Mach number 2.85 at an altitude of 68,000 feet, with a 70-percent diffuser recovery giving a burner-inlet pressure of 1 atmosphere and temperature of 570 degree Fahrenheit" (p. 1).
Date: June 1, 1955
Creator: Kerslake, William R.; Dangle, E. E. & Cervenka, A. J.
Object Type: Report
System: The UNT Digital Library
Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic (open access)

Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic

Report presenting an exploration of the proposition that the structural weight of supersonic missiles should be reduced by the use of pressurized, thin-wall, glass-laminated shells. A model with this type of structure was investigated in the 8- by 6-foot supersonic wind tunnel to determine the minimum internal pressure necessary to prevent panel flutter. Results regarding the empty shell and shell containing liquid are provided.
Date: June 1, 1955
Creator: Leissler, L. Abbott
Object Type: Report
System: The UNT Digital Library
Radioactivity Transport in Water: the Dispersion of Radionuclides in Open Channel Flow (open access)

Radioactivity Transport in Water: the Dispersion of Radionuclides in Open Channel Flow

From introduction: It is the purpose of this study to present field measurements of dispersion in a river and a canal, whose characteristics are unlike streams in which similar work has been done. The Colorado River and the Pierce Canal were selected for testing.
Date: June 1, 1963
Creator: Patterson, Calvin Clyde & Floyna, Earnest F.
Object Type: Report
System: The UNT Digital Library
The Effect of Crystallite Size on the Bulk Density and Strength Properties of Uranium Dioxide Specimens (open access)

The Effect of Crystallite Size on the Bulk Density and Strength Properties of Uranium Dioxide Specimens

Fused uranium dioxide was separated into fractions of varying particle size by air separation. Specimens of the nominal size of 1/8 by 1/4 by 1½ in. were formed by hydrostatic pressing, firing, and lapping. Specimens prepared from the 0 to 5 μ fraction were the strongest and most dense. The room-temperature density was about 92% of theoretical and the room-temperature flexural strength was about 12,000 1b. per sq. in. When tested at 1000°C., the strength was about 18,000 1b. per sq. in. The flexural strength of specimens decreased and their density decreased as the starting particle size was increased. The crystallization of the urania fragments which had occurred during the firing treatment was observed.
Date: June 1, 1955
Creator: Burdick, Milton D. & Parker, H. S.
Object Type: Report
System: The UNT Digital Library
Determination of half life of polonium-210 by counting: final report (open access)

Determination of half life of polonium-210 by counting: final report

Introduction: "A number of determination have been made of the half life of polonium-210 by calorimetry. Counting affords an entirely different method of determining half lives and requires only a small amount of activity. Therefore for comparison a half-life determination by counting was undertaken with a sample of approximately 0.5 millicurie of polonium."
Date: June 1, 1951
Creator: Curtis, Mary Lou
Object Type: Report
System: The UNT Digital Library
Coupled Transmission Lines (open access)

Coupled Transmission Lines

In a discussion about design of cyclotron resonators, the suggestion has been made that a wide range variable-frequency system might be constructed with two coupled resonant circuits. It also would present the possibility of tuning without the switching of high-current contacts, a troublesome item now commonly used for cyclotrons. One of the circuits would be the dee and its stem which might, or might not, be tuned. The second circuit could be located out of the magnet gap in a region where more space is usually available. Tuning could be accomplished by variation of the coupling between the two circuits and/or by, say, variable capacitance of the tuned, or tunable, circuit.
Date: June 1, 1959
Creator: Worsham, R. E. & Mosko, S. W.
Object Type: Report
System: The UNT Digital Library
Nuclear Safety of Right Elliptic and Right Annular Cylinders (open access)

Nuclear Safety of Right Elliptic and Right Annular Cylinders

Past experience has shown that the demand for increase separations plant capacity comes up very regularly. One of the variables which greatly affects plant capacity is cross-sectional area of the individual vessels. Larger areas permit greater flow rates as well as more space for the installation of heat transfer piping (shell and tube concentrators). Design considerations of the separations plants vessels have been based on both circular cylinder and slab geometries. A study has been made to determine other vessel geometries that will result in safe vessels from a nuclear safety standpoint and at the same time offer larger cross-sectional areas than right circular cylinders. Vessels of elliptic as well as annular cross sections have been considered. It is neither the intent of this study to discuss the effects of intersection, vessel piping, etc., nor the pros and cons of fabricating feasibility and structural strength of these different shaped vessels. The main purpose is to make comparisons of cross-sectional areas (capacity parameter) of safe vessels so that vessel shape may be evaluated as one of the parameters in any design study for separation plants.
Date: June 1, 1956
Creator: Ketzlach, Norman
Object Type: Report
System: The UNT Digital Library
Progress Relating to Civilian Applications During May, 1956 (open access)

Progress Relating to Civilian Applications During May, 1956

A report about mechanical properties of dilute uranium alloys are being investigated in an effort to develop a high-strength alloy for fuel elements. Elevated temperature tensile tests were made on two dilute uranium-aluminum alloys, and several ternary alloys were arc melted.
Date: June 1, 1956
Creator: Dayton, Russell W. & Tipton, Clyde R., Jr.
Object Type: Report
System: The UNT Digital Library