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[Investigation Report from George Woods, March 21, 1943] (open access)

[Investigation Report from George Woods, March 21, 1943]

Investigation Report from George Woods containing a copy of an attached signed statement by one Logan Pierson for the case of U.S. vs. Plosser et al.
Date: March 21, 1943
Creator: Woods, George
System: The Portal to Texas History
Technical Department report on Production Test No. 313-62-M: Effect of bar position on seating in the canning of heavy metal slugs (open access)
Effect of combustor-inlet conditions on performance of an annular turbojet combustor (open access)

Effect of combustor-inlet conditions on performance of an annular turbojet combustor

From Summary: "The combustion performance, and particularly the phenomenon of altitude operational limits, was studied by operating the annular combustor of a turbojet engine over a range of conditions of air flow, inlet pressure, inlet temperature, and fuel flow. Information was obtained on the combustion efficiencies, the effect on combustion of inlet variables, the altitude operational limits with two different fuels, the pressure losses in the combustor, the temperature and velocity profiles at the combustor outlet, the extent of afterburning, the fuel-injection characteristics, and the condition of the combustor basket."
Date: March 21, 1947
Creator: Childs, J. Howard; McCafferty, Richard J. & Surine, Oakley W.
System: The UNT Digital Library
METHODS FOR THE ANALYSIS OF BERYLLIUM CARBIDE (open access)

METHODS FOR THE ANALYSIS OF BERYLLIUM CARBIDE

Analytical methods are given for determining the composition and impurities of beryllium carbide. A summary of the experimental work leading to these procedures and supporting data are also presented. Analytical procedures for the determination of free and combined carbon, moisture, nitrogen, beryllium oxide, silica, iron, total beryllium, and beryllium metal are outlined. Diagrams of special apparatus used are included. (auth)
Date: March 21, 1949
Creator: Bridges, W.L.; Funston, E.S. & Reed, S.A.
System: The UNT Digital Library
On Stability of Free Laminar Boundary Layer Between Parallel Streams (open access)

On Stability of Free Laminar Boundary Layer Between Parallel Streams

"An analysis and calculations on the stability of the free laminar boundary layer between parallel streams were made for an incompressible fluid using the Tollmien-Schlichting theory of small disturbances. Because the boundary conditions are at infinity, two solutions of the Orr-Sommerfeld stability equations need not be considered, and the remaining two solutions are exponential in character at the infinite boundaries. The calculations show that the flow is unstable except for very low Reynolds numbers" (p. 571).
Date: March 21, 1949
Creator: Lessen, Martin
System: The UNT Digital Library
Attenuation of Gamma Radiation by High Density Lead Glass Compared With Steel (open access)

Attenuation of Gamma Radiation by High Density Lead Glass Compared With Steel

None
Date: March 21, 1950
Creator: Wheeler, R. G.
System: The UNT Digital Library
Cooling of ram jets and tail-pipe burners: analytical method  for determining temperatures of combustion chamber having annular cooling passage (open access)

Cooling of ram jets and tail-pipe burners: analytical method for determining temperatures of combustion chamber having annular cooling passage

Report presenting an analytical method for calculating the maximum wall temperature of a tail-pipe burner or a ramjet combustion chamber cooled by air or gas flowing through a surrounding annular passage.
Date: March 21, 1950
Creator: Koffel, William K.; Stamper, Eugene & Sanders, Newell D.
System: The UNT Digital Library
The Effect of the Inlet Mach Number and Inlet-Boundary-Layer Thickness on the Performance of a 23 Degree Conical-Diffuser-Tail-Pipe Combination (open access)

The Effect of the Inlet Mach Number and Inlet-Boundary-Layer Thickness on the Performance of a 23 Degree Conical-Diffuser-Tail-Pipe Combination

An investigation was conducted to determine the effect of the inlet Mach number and entrance-boundary-layer thickness on the performance of a 23 degree 21-inch conical-diffuser - tail-pipe combination with a 2:1 area ratio. The air flows used in this investigation covered an inlet Mach number range from 0.17 to 0.89 and corresponding Reynolds numbers of 1,700,000 to 7,070,000. Results are reported for two inlet-boundary-layer thicknesses.
Date: March 21, 1950
Creator: Persh, Jerome
System: The UNT Digital Library
Statistical evaluation of calibrartion data-infrared method for determination of % TBP (open access)

Statistical evaluation of calibrartion data-infrared method for determination of % TBP

A report which discusses the data submitted for evaluation. This data is about optical densities from infrared spectrometer readings on eight standard samples, ranging in percent TBP from 6.71 to 17.85.
Date: March 21, 1950
Creator: Healy, W. C.
System: The UNT Digital Library
Health - Physics Monthly Information Report. February 1-28, 1951 (open access)

Health - Physics Monthly Information Report. February 1-28, 1951

None
Date: March 21, 1951
Creator: Boozer, A. H.
System: The UNT Digital Library
Review of Problems of Conservation of Strategic Materials for Turbine Engines (open access)

Review of Problems of Conservation of Strategic Materials for Turbine Engines

Memorandum presenting a discussion of the strategic-material problems of airplane engines as a whole, especially as related to parts of the engine that are not the disk or blades. Several possible approaches to the material-conservation problem are presented, including the advantages and disadvantages, and the relative gains that might result from one, or combination of a number, of these approaches.
Date: March 21, 1951
Creator: Materials Research Staff
System: The UNT Digital Library
An analysis of once-per-revolution oscillating aerodynamic thrust loads on single-rotation propellers on tractor airplanes at zero yaw (open access)

An analysis of once-per-revolution oscillating aerodynamic thrust loads on single-rotation propellers on tractor airplanes at zero yaw

A simplified procedure is shown for calculating the once-per-revolution oscillating aerodynamic thrust loads on propellers of tractor airplanes at zero yaw. The only flow field information required for the application of the procedure is a knowledge of the upflow angles at the horizontal center line of the propeller disk. Methods are presented whereby these angles may be computed without recourse to experimental survey of the flow field. The loads computed by the simplified procedure are compared with those computed by a more rigorous method and the procedure is applied to several airplane configurations which are believed typical of current designs. The results are generally satisfactory.
Date: March 21, 1955
Creator: Rogallo, Vernon L.; Yaggy, Paul F. & McCloud, John L., III
System: The UNT Digital Library
The Photosynthetic Cycle (open access)

The Photosynthetic Cycle

None
Date: March 21, 1955
Creator: Calvin, Melvin
System: The UNT Digital Library
Transient Temperature Variations During the Self-Heating of a Plasma by Thermonuclear Reactions (open access)

Transient Temperature Variations During the Self-Heating of a Plasma by Thermonuclear Reactions

Abstract: "The possibility of transient temperature variations during the self-heating of a plasma by thermonuclear reactions was investigated. Calculations were performed on an IBM Card Program Calculator. Estimates of the time scale for self-heating were obtained. It was concluded that it would be unsafe to assume that the nuclear temperature is always equal to or greater than the electron temperature in a discussion of plasma instabilities for a plasma with 10 percent or greater tritium concentration."
Date: March 21, 1955
Creator: Greyber, Howard D.
System: The UNT Digital Library
Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 (open access)

Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

"A program to investigate the aerodynamic heat transfer of a nonisothermal hemisphere-cylinder has been conducted in the Langley 11-inch hypersonic tunnel at a Mach number of 6.8 and a Reynolds number from approximately 0.14 x 10(6) to 1.06 x 10(6) based on diameter and free-stream conditions. The experimental heat-transfer coefficients were slightly less over the whole body than those predicted by the theory of Stine and Wanlass (NACA technical note 3344) for an isothermal surface. For stations within 45 degrees of the stagnation point the heat-transfer coefficients could be correlated by a single relation between local Stanton number and local Reynolds number" (p. 1001).
Date: March 21, 1956
Creator: Crawford, Davis H. & McCauley, William D.
System: The UNT Digital Library
PROGRAM FOR THE HRT CORE PROCESSING PLANT (open access)

PROGRAM FOR THE HRT CORE PROCESSING PLANT

None
Date: March 21, 1956
Creator: Lindauer, R B
System: The UNT Digital Library
Anisotropic Elastic Scattering of Neutrons (open access)

Anisotropic Elastic Scattering of Neutrons

In an elastic collision the neutron loses part of its kinetic energy to the nucleus with both the kinetic and momentum of the system being conserved. However, for many elements the scattering is not isotropic in the center-of-mass system at the higher neutron energies. Many of the present reactor multigroup codes include anisotropic scattering at the high neutron energies, while many others assume isotropic scattering at all energies. In order to consider some of the effects of including anisotropic scatting, reference is made t the multigroup equation generally assumed for the slowing-down density.
Date: March 21, 1957
Creator: Copenhaver, C. M.
System: The UNT Digital Library
Beryllium (open access)

Beryllium

The information concerning beryllium assembled herein has been selected primarily to provide information that might be pertinent to the design of the ART. The creep-rupture data in the literature have been obtained from vacuum cast and extruded beryllium, rather than from the hot-pressed beryllium which will be used in the ART. A research program is being conducted by the Brush Beryllium Company, under contract to the Oak Ridge National Laboratory, which will eventually provide the design engineers with data on the high temperature strength properties of hot-pressed beryllium. In the interim, it will be necessary for the metallurgists and design engineers to make judicious estimates and extrapolations from the data available.
Date: March 21, 1957
Creator: Whitman, M. J.
System: The UNT Digital Library
Chemical Processing Department Monthly Report: February 1957 (open access)

Chemical Processing Department Monthly Report: February 1957

This report from the Chemical Processing Department at HAPO, discusses the following: Production operation, purex operation, redox operation, finished products operation, power and general maintenance operation, financial operation, facilities engineering operation, research and engineering operation, and employee relations operation.
Date: March 21, 1957
Creator: Hanford Atomic Products Operation. Chemical Processing Department.
System: The UNT Digital Library
Exploratory Drilling in the Nash Car Locality, White Canyon Area, San Juan County, Utah (open access)

Exploratory Drilling in the Nash Car Locality, White Canyon Area, San Juan County, Utah

Gregory described the broad geologic and geographic features of the white canyon area in the reconnaissance report on San Juan county.
Date: March 21, 1957
Creator: Oertell, E. W. & Spencer, D. F
System: The UNT Digital Library
Some Effects of Variation in Exposure Time and Input Pulse Shape in the Production of Radiant Energy Thermal Burns (open access)

Some Effects of Variation in Exposure Time and Input Pulse Shape in the Production of Radiant Energy Thermal Burns

None
Date: March 21, 1957
Creator: Payne, F. W. & Hinshaw, J. R.
System: The UNT Digital Library
Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations (open access)

Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations

Report discussing an investigation to determine the effect of spin on the aerodynamic characteristics of the Army Ordnance Corps 60-millimeter T-24 mortar shell with several tail-fin configurations. Tests were performed at several airspeeds, speeds of rotation, and angles of attack. Under all test conditions, the models were statistically stable and the yawing moment increased with speed of rotation at higher angles of attack.
Date: March 21, 1957
Creator: Kemp, William B., Jr. & Hayes, William C., Jr.
System: The UNT Digital Library
Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations (open access)

Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell With Several Tail-Fin Configurations

Report presenting an investigation in the high-speed tunnel to determine the effect of spin on the aerodynamic characteristics of a 60-millimeter T-24 mortar shell with several different tail-fin configurations. Tests were made at a range of airspeeds, speeds of rotation, and angles of attack. Results regarding forced-spin tests, free-spin tests, and zero-spin tests are provided.
Date: March 21, 1957
Creator: Kemp, William B., Jr. & Hayes, William C., Jr.
System: The UNT Digital Library
Chemical Processing Department monthly report, February 1958 (open access)

Chemical Processing Department monthly report, February 1958

The February, 1958 monthly report for the Chemical Processing Department of the Hanford Atomic Products Operation includes information regarding research and engineering efforts with respect to the Purex and Redox process technology. Also discussed is the production operation, finished product operation, power and general maintenance, financial operation, engineering and research operations, and employee operation. (MB)
Date: March 21, 1958
Creator: unknown
System: The UNT Digital Library