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Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine (open access)

Comparison of flight performance of AN-F-58 and AN-F-32 fuels in J35 turbojet engine

Report presenting a flight investigation to determine the comparative performance of AN-F-58 and AN-F-32 fuels in a 4000-pound-thrust turbojet engine. The fuels were equivalent over the range of conditions investigated. Results regarding corrected net thrust, corrected jet-fuel consumption, variation of corrected tail-pipe temperature, combustor blow-out speeds, and visual observations of the jet exhaust are provided.
Date: April 7, 1949
Creator: Acker, Loren W. & Kleinknecht, Kenneth S.
System: The UNT Digital Library
Health problems associated with investigation of off-plant uranium rolling. Rough draft (open access)

Health problems associated with investigation of off-plant uranium rolling. Rough draft

The following is a report of a trip to the Simonds Saw & Steel Company, Lockport, New York, on May 3, 1949. The purpose of the visit was to observe the various operations involved in the rolling of uranium rods at this plant and health problems associated with the rolling operations.
Date: May 13, 1949
Creator: Adley, F. E.
System: The UNT Digital Library
Oxides of nitrogen exposures accompanying pickling operations 313 Building - 300 Area (open access)

Oxides of nitrogen exposures accompanying pickling operations 313 Building - 300 Area

None
Date: March 11, 1949
Creator: Adley, F. E.
System: The UNT Digital Library
Reduction of oxides of nitrogen exposures at pickling operation, 313 Building, 300 area (open access)

Reduction of oxides of nitrogen exposures at pickling operation, 313 Building, 300 area

None
Date: December 5, 1949
Creator: Adley, F. E.
System: The UNT Digital Library
A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods (open access)

A Comparison of Wing Loads Measured in Flight on a Fighter-Type Airplane by Strain-Gage and Pressure Distribution Methods

Note presenting pressure distribution measurements made on the wing of a fighter-type airplane to determine the span loading and to compare center-of-pressure results with those obtained by strain-gage measurements on the same airplane during a previous flight investigation. Flight tests were all made at a pressure altitude of about 30,000 feet and covered a Mach number range from approximately 0.35 to 0.81. Results regarding additional air load, spanwise center of pressure of additional air load, basic air load distribution, and span loading during a stall and buffeting are provided.
Date: November 1949
Creator: Aiken, William S., Jr. & Howard, Donald A.
System: The UNT Digital Library
Polarographic Analysis of UNH in the IAW Stream (open access)

Polarographic Analysis of UNH in the IAW Stream

The following report describes two rapid, micro methods for the determination of UNH in Redox waste samples that had been developed fir the concentration range 0.2 to 100 g/l.
Date: January 17, 1949
Creator: Alkire, G. J. & Carson, W. N.
System: The UNT Digital Library
Polarographic Determination of Hexone (open access)

Polarographic Determination of Hexone

The following report describes polarographic methods that determine saturated aliphatic carbonyl compounds.
Date: November 10, 1949
Creator: Alkire, George J.
System: The UNT Digital Library
DECOMPOSITION OF WATER AND AQUEOUS SOLUTIONS UNDER PILE RADIATION (open access)

DECOMPOSITION OF WATER AND AQUEOUS SOLUTIONS UNDER PILE RADIATION

None
Date: October 11, 1949
Creator: Allen, A. O.; Davis, T. W.; Elmore, G. V.; Ghormley, J. A.; Haines, B. M. & Hochanadel, C. J.
System: The UNT Digital Library
Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio (open access)

Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio

Report presenting a discussion of the aerodynamic forces and moments on inclined bodies of revolution. An approximate theory to allow for the effects of viscosity is developed and applied. Results regarding the variation of lift and pitching moment, and center of gravity are provided.
Date: November 14, 1949
Creator: Allen, H. Julian
System: The UNT Digital Library
Investigation of Sublette Ridge Vanadium Deposit, Lincoln County, Wyoming (open access)

Investigation of Sublette Ridge Vanadium Deposit, Lincoln County, Wyoming

Report issued by the Bureau of Mines over studies conducted on vanadium deposits in Lincoln County. As noted in the introduction, "the following report covers the history of the district, outlines the physical features and communications, mentions the property, and notes the ownership. The deposits and ore are described, and work performed by the Bureau of Mines is explained in detail" (p. 1). This report includes tables, and maps.
Date: June 1949
Creator: Allsman, Paul T.; Majors, Forest H.; Mahoney, Stanford R. & Young, W. A.
System: The UNT Digital Library
Investigations of Salt River Vanadium Deposits, Lincoln County, Wyoming (open access)

Investigations of Salt River Vanadium Deposits, Lincoln County, Wyoming

Report issued by the Bureau of Mines over studies conducted on the vanadium deposits of Lincoln County, Wyoming. As stated in the introduction, "the work performed by the Bureau of Mines is explained in detail and supplemented with plans, sections, and a complete set of sample analyses. Proposed mining methods are discussed, and metallurgical tests are outlined" (p. 2). This report includes tables, maps, and illustrations.
Date: August 1949
Creator: Allsman, Paul T.; Majors, Forest H.; Mahoney, Stanford R. & Young, W. A.
System: The UNT Digital Library
Limits of Inflammability and Ignition Temperatures of Hexone in Air and in Other Gaseous Atmospheres (open access)

Limits of Inflammability and Ignition Temperatures of Hexone in Air and in Other Gaseous Atmospheres

The following report summarizes the data taken from a series of measurements on the combustion and ignition properties of hexone. The experiments were taken at the Bureau of Mines Central Experiment Station by their personnel, and the samples were given to them by KAPL and Hanford.
Date: September 9, 1949
Creator: Alter, H. Ward
System: The UNT Digital Library
Nitrogen 12 (open access)

Nitrogen 12

N{sup 12} is shown to have a half life of 12.5 {+-} 1 milliseconds, and a positron upper limit of 16.6 {+-} 0.2 Mev. It is produced by the reaction C{sup 12}(p,n)N{sup 12}, and has a threshold proton energy of 20.0 Mev. This indicates that N{sup 12} is within about 200 Kev of being unstable against proton emission. The mass of N{sup 12} is 12.0228 {+-} 0.00015, and the beta transition is allowed.
Date: January 19, 1949
Creator: Alvarez, Luis W.
System: The UNT Digital Library
A Proposed Experimental Test of the Neutrino Theory (open access)

A Proposed Experimental Test of the Neutrino Theory

The experiment outlined in this proposal has the possibility of giving an answer to the important question, 'Does the neutrino exist'? It is unfortunate that at the present time, there is no convincing experimental that neutrinos exist. Two recent articles review the status of various experiments which could give information about neutrinos. In general, these experiments give results in agreement with the predictions of beta decay theory. But actually, if even the most complete of the 'recoil type' experiments could be performed satisfactorily, all that could be concluded would be the following: the energy and momentum relationships in beta decay are consistent with the theory that the known energy deficit is carried away by a single particle. But to emphasize the fact that this would not constitute a proof of the real existence of that particle, the following quotations from the review articles should be noted. Crane says, 'All of the evidence about the neutrino is, as already pointed out, indirect in character since neutrinos have not yet been caught after leaving the nucleus. It can, of course, be argued on very general grounds that, if energy is not conserved between nucleus and electron, momentum should not be expected to …
Date: April 18, 1949
Creator: Alvarez, Luis W.
System: The UNT Digital Library
Chordwise and Spanwise Loadings Measured at Low Speed on Large Triangular Wings (open access)

Chordwise and Spanwise Loadings Measured at Low Speed on Large Triangular Wings

Report presenting pressure distributions of three triangular wing models: a wing-alone model, the same wing combined with a body, and a mock-up of a triangular-wing airplane. Results regarding the separation-vortex air flow over triangular wings, general comments regarding the applicability of the study, chordwise pressure distribution, section lift characteristics, center of pressure, and span load distribution are provided.
Date: April 19, 1949
Creator: Anderson, Adrien E.
System: The UNT Digital Library
An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 3: Characteristics of Wing With Body and Vertical Tail (open access)

An Investigation at Low Speed of a Large-Scale Triangular Wing of Aspect Ratio Two 3: Characteristics of Wing With Body and Vertical Tail

Report presenting an investigation to determine the aerodynamic characteristics in sideslip of a triangular wing of aspect ratio 2.04 in combination with a body of fineness ratio 12.5 and a vertical tail surface. The body combined with the triangular plan-form wing caused no significant changes in the lift characteristics of the wing and only a 1-percent decrease in the static margin. Results regarding the longitudinal characteristics, lateral and directional characteristics, and estimation of tail and rudder effectiveness are provided.
Date: October 14, 1949
Creator: Anderson, Adrien E.
System: The UNT Digital Library
Fabrication of Uranium Wire (open access)

Fabrication of Uranium Wire

From abstract: "The present report describes experimental work performed to establish a procedure for the production of uranium metal wire. In all cases, the size of the initial rod was 1/2 inch diameter. Three materials were used: hot extruded tuballoy rod, high purity cast tuballoy rod, and cast U-235 rod."
Date: October 25, 1949
Creator: Anderson, R. E.; Taub, J. M. & Doll, D. T.
System: The UNT Digital Library
FABRICATION OF URANIUM WIRE (open access)

FABRICATION OF URANIUM WIRE

None
Date: October 25, 1949
Creator: Anderson, R.E.; Taub, J.M. & Doll, D.T.
System: The UNT Digital Library
Quarterly Report February, March, April, 1949: Biological and Medical Divisions (open access)

Quarterly Report February, March, April, 1949: Biological and Medical Divisions

Report issued by the Argonne National Laboratory discussing the progress and work completed between February and April, 1949. Descriptions of the studies conducted and progress made are presented. This report includes tables, illustrations, and photographs.
Date: 1949-03/1949-04
Creator: Argonne National Laboratory
System: The UNT Digital Library
Reactor Engineering Division Quarterly Report, June 1, 1949 - August 31, 1949 (open access)

Reactor Engineering Division Quarterly Report, June 1, 1949 - August 31, 1949

Report issued by the Argonne National Laboratory covering the quarterly report from the Reactor Engineering Division. A summary of reactor programs, designs, development, and experiments are presented. This report includes tables, illustrations, and photographs.
Date: October 7, 1949
Creator: Argonne National Laboratory. Reactor Engineering Division.
System: The UNT Digital Library
The Machinability of Beryllium (open access)

The Machinability of Beryllium

The following report investigates the isolation of the cause of the unusual tool-wear rates found in machining beryllium as attributed to an inherent characteristic of beryllium, or an effect of inclusions in beryllium, as well as the evaluation of the comparative machinability of the various types of beryllium.
Date: April 30, 1949
Creator: Armstrong, E. T.; Dayton, Russell Wendt & Dawes, R. C.
System: The UNT Digital Library
Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle (open access)

Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 2: 18.41-Inch-Diameter Jet Nozzle

Report presenting an altitude-chamber investigation to determine the altitude performance characteristics of the British Rolls-Royce Nene II turbojet engine with an 18.41-inch-diameter jet nozzles. Testing occurred at a range of simulated altitudes and ram-pressure ratios. Results regarding the simulated flight performance, generalized performance, and effect of jet-nozzle area on performance are provided.
Date: October 26, 1949
Creator: Armstrong, J. C.; Wilsted, H. D. & Vincent, K. R.
System: The UNT Digital Library
Extrusion ar Revere Copper and Brass, Inc., March 1, 1949 (open access)

Extrusion ar Revere Copper and Brass, Inc., March 1, 1949

None
Date: March 1, 1949
Creator: Arnold, S. V.
System: The UNT Digital Library
Bare Beryllium Extrusion Using Graphite Introductory Cones (open access)

Bare Beryllium Extrusion Using Graphite Introductory Cones

The following document describes the process of rare beryllium extrusion using graphite introductory cones with the purpose of finding a lubricant which would decrease excessive friction between the billet and prose parts.
Date: June 28, 1949
Creator: Arnold, Samuel V.
System: The UNT Digital Library