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A Microdetermination of Uranium by Ferric Sulfate Titration (open access)

A Microdetermination of Uranium by Ferric Sulfate Titration

Abstract: "Following nitrate removal by means of a three-stage hydrochloric acid digestion, uranium was reduced with chromous sulfate reagent. In an inert atmosphere, the quadrivalent uranium was titrated at 80-95[degrees] with standard ferric sulfate solution. The end point was obtained with a potentiometric cell including a platinum in-titrant reference electrode and a platinum indicator electrode. Application was made to various low leverl uranium solutions. For samples containing 1 - 12 milligrams or uranium, less than one percent error may be expected. Iron and chromium do not interfere."
Date: February 16, 1949
Creator: Christopherson, E. W.
System: The UNT Digital Library
The Coulometric Titration of 8-Hydroxyquinoline (open access)

The Coulometric Titration of 8-Hydroxyquinoline

Abstract: "A new method of determining 8-hydroxyquinoline by titration with electrolytucally-generated bromine has been developed. Results show good precision in the range 0.4 mg. to 1.6 mg. total 8-hydroxyquinoline, with 99% confidence limits of less than +/- 2%. An electronically-regulated constant current source, required by the method, is described. A new indicator system with high sensitivity to free bromine is discussed."
Date: June 16, 1949
Creator: Carson, W. N.
System: The UNT Digital Library
The Coulometric Determination of Acetic Acid (open access)

The Coulometric Determination of Acetic Acid

Abstract: "Small amounts of acetic acid, equivalent to 400 ul. of 0.3 to 0.13 g/L. can be titrated coulonatrically in the presence of a 10 to 25-fold excess of HN03 in 70%, isopropanol. An accuracy of +/- 0.1% and a precision of +/- 8.5% (99% limite) are obtained.
Date: August 16, 1949
Creator: Carson, W. N. & Ko, Roy
System: The UNT Digital Library
Redox Committee: Conference notes and recommendations, meeting of May 16, 1949 (open access)

Redox Committee: Conference notes and recommendations, meeting of May 16, 1949

None
Date: May 16, 1949
Creator: Greager, O. H.; MacCready, W. K. & Seckendorff, E. W.
System: The UNT Digital Library
The present status of polonium tolerance estimation. Biology seminar, February 1, 1949 (open access)

The present status of polonium tolerance estimation. Biology seminar, February 1, 1949

Despite the fact the adequate data from long-term, chronic experiments on the effects of Po{sup 210} are not available, some sort of a working figure for the maximum permissible body content of polonium is desirable. As described herein, calculations involved in determining the permissible body content of polonium generally fall into three classes. 1. Comparison of X-ray and polonium toxicity and application of an acceptable X-ray tolerance figure. 2. Assumption of a most sensitive organ and computation of the critical concentration of radioactive material present in this organ under conditions such that the organ received an assumed maximum permissible exposure over an indefinitely long period of time. 3. Comparison of radium and polonium toxicity with application of an acceptable maximal content of radium.
Date: February 16, 1949
Creator: Hackett, P. L.
System: The UNT Digital Library
Information for Reactor Safeguard Committee (open access)

Information for Reactor Safeguard Committee

This report provides information on reactivity, temperature coefficients and energy storage to the Reactor Safeguard Committee with regard to contemplated increases in power levels.
Date: November 16, 1949
Creator: Woods, W. K.
System: The UNT Digital Library
100 Areas technical activities report: Physics, November 1949 (open access)

100 Areas technical activities report: Physics, November 1949

Work of the pile physics and experimental physics groups is reported. Theoretical work is also reported.
Date: November 16, 1949
Creator: Carson, A. B.
System: The UNT Digital Library
Decomposition of Water at High Temperatures and Pressures Under Reactor Irradiation (open access)

Decomposition of Water at High Temperatures and Pressures Under Reactor Irradiation

Partial abstract: "The investigation of the high temperature and pressure dissociation of water under irradiation was undertaken by the Power Pile Division of Oak Ridge National Laboratory in an effort to determine the degree of importance of the phenomenon with respect to the design of a high temperature water-cooled power reactor. Theory and past experimentation indicate that net steady-state dissociation is determined by the rates of the dissociation and recombination reactions under the imposed conditions, the dissociation rate being essentially a function of flux and the recombination rate essentially a function of temperature" (p. 3).
Date: September 16, 1949
Creator: Fromm, L. W.
System: The UNT Digital Library
The Spectrochemical Analysis of Hafnium and Zirconium (open access)

The Spectrochemical Analysis of Hafnium and Zirconium

Abstract: "The analysis of hafnium and zirconium by the copper spark technique is presented for solutions of HCl, HF, and HClO4 acids. The special techniques of electrode protection and vacuum drying of perchloric acid samples are outlined. Also given are the working curves and deviations of both elements."
Date: March 16, 1949
Creator: Conway, John G. & Moore, Milton F.
System: The UNT Digital Library
Some Notes on Wideband Feedback Amplifiers (open access)

Some Notes on Wideband Feedback Amplifiers

The extension of the passband of wideband amplifiers is a highly important problem to the designer of electronic circuits. Throughout the electronics industry and in many research programs in physics and allied fields where extensive use is made of video amplifiers, the foremost requirement is a passband of maximum width. This is necessary if it is desired to achieve a more faithful reproduction of transient wave forms, a btter time resolution in physical measurements, or perhaps just a wider band gain-frequency response to sine wave signals. The art of electronics is continually faced with this omnipresent amplifier problem. In particular, the instrumentation techniques of nuclear physics require amplifiers with short rise times, a high degree of gain stability, and a linear response to high signal levels. While the distributed amplifier{sup 1} may solve the problems of those seeking only a wide passband, the requirements of stability and linearity necessitate using feedback circuits. This paper considers feedback amplifiers from the standpoint of high-frequency performance. The circuit conditions for optimum steady-state (sinusoidal) and transient response are derived and practical circuits (both interstage and output) are presented which fulfill these conditions. In general, the results obtained may be applied to the low-frequency end. …
Date: March 16, 1949
Creator: Fitch, V.
System: The UNT Digital Library
Determination of Rate, Area, and Distribution of Impingement of Waterdrops on Various Airfoils From Trajectories Obtained on the Differential Analyzer (open access)

Determination of Rate, Area, and Distribution of Impingement of Waterdrops on Various Airfoils From Trajectories Obtained on the Differential Analyzer

"The trajectories of waterdrops in air flowing over airfoils are determined for three airfoil - angle-of-attack combinations using the differential analyzer to solve the differential equations of motion of the waterdrops. From these trajectories the rate of water impingement, the area of impingement, and the distribution of impingement are determined as functions of two dimensionless moduli. Comparisons are made of the rate of water impingement on these airfoils and the rate of water impingement on cylinders" (p. 1).
Date: February 16, 1949
Creator: Guibert, A. G.; Janssen, E. & Robbins, W. M.
System: The UNT Digital Library
Determination of rate, area, and distribution of impingement of of waterdrops on various airfoils from trajectories obtained on the differential analyzer (open access)

Determination of rate, area, and distribution of impingement of of waterdrops on various airfoils from trajectories obtained on the differential analyzer

From Summary: "The trajectories of waterdrops in air flowing over airfoils are determined for three airfoil-angle-of-attack combinations using the differential analyzer to solve the differential equations of motion of the waterdrops. From these trajectories the rate of water impingement, the area of impingement, and the distribution of impingement are determined as functions of two dimensionless moduli. Comparisons are made of the rate of water impingement on these airfoils and the rate of water impingement on cylinders."
Date: February 16, 1949
Creator: Guibert, A. G.; Janssen, E. & Robbins, W. M.
System: The UNT Digital Library
Determination of rate, area, and distribution of impingement of water drops on various airfoils from trajectories obtained on the differential analyzer (open access)

Determination of rate, area, and distribution of impingement of water drops on various airfoils from trajectories obtained on the differential analyzer

From Summary: "The trajectories of waterdrops in air flowing over airfoils are determined for three airfoil-angle-of-attack combinations using the differential analyzer to solve the differential equations of motion of the waterdrops. From these trajectories the rate of water impingement, the area of impingement, and the distribution of impingement are determined as functions of two dimensionless moduli. Comparisons are made of the rate of water impingement on these airfoils and the rate of water impingement on cylinders."
Date: February 16, 1949
Creator: Guibert, A. G.; Janssen, E. & Robbins, W. M.
System: The UNT Digital Library
Flight Investigation of Flutter Models With 1/10-Scale Douglas D-558-2 Wing Panels (open access)

Flight Investigation of Flutter Models With 1/10-Scale Douglas D-558-2 Wing Panels

Report presenting testing of three rocket-powered models with Douglas D-558-2 wings as horizontal fins with scaled structural parameters to determine whether the possibility of wing flutter due to torsion and bending exists in full-scale airplanes at transonic speeds. No wing flutter was present in the models tested, but pitching oscillation developed as it passed into the transonic range.
Date: February 16, 1949
Creator: Teitelbaum, Jerome M.
System: The UNT Digital Library
Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges (open access)

Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges

Memorandum presenting an exploratory investigation to determine the aerodynamic effects of camber on a 60 degree apex delta-wing model conducted in the 300 mph 7- by 10-foot tunnel. Camber variation was accomplished through the deflection of full-span round and 25 degree beveled leading-edge flaps on a flat-sided triangular plan-form wing.
Date: August 16, 1949
Creator: Riebe, John M. & Fikes, Joseph E.
System: The UNT Digital Library
Study of the canard configuration with particular reference to transonic flight characteristics and low-speed characteristics at high lift (open access)

Study of the canard configuration with particular reference to transonic flight characteristics and low-speed characteristics at high lift

Report presenting a study of the flight characteristics of the canard configuration at transonic and supersonic speeds. Known problems concerning the low-speed characteristics of the canard are also investigated.
Date: November 16, 1949
Creator: Mathews, Charles W.
System: The UNT Digital Library
Effect of hot-gas bleedback ice prevention on performance of a turbojet engine with fixed-area tail-pipe nozzle (open access)

Effect of hot-gas bleedback ice prevention on performance of a turbojet engine with fixed-area tail-pipe nozzle

Report presenting the results of an analytical investigation, which demonstrated that the inlet of a turbojet engine can be protected from ice accretions by bleeding hot gases from other locations within the engine to the inlet without undue loss in thrust. Results regarding the bleedback requirements, engine performance, effect of nozzle area, mixing efficiency, and seriousness of thrust losses are provided.
Date: May 16, 1949
Creator: Dietz, Robert O., Jr. & Krebs, Richard P.
System: The UNT Digital Library
Power Recovery at Brookhaven ; Report No. 1 (open access)

Power Recovery at Brookhaven ; Report No. 1

From introduction: "This is the first report on the study made of the possible power recovery without excessive cost, from the operation of the Brookhaven reactor."
Date: June 16, 1949
Creator: Lucke, Charles Edward
System: The UNT Digital Library
Direct Reduction of Uranium Hexafluoride to Metallic Uranium (open access)

Direct Reduction of Uranium Hexafluoride to Metallic Uranium

Exploratory tests are reported which indicate the feasibility of a one-step reduction process for the preparation of uranium metal from the hexafluoride by the action of calcium metal and iodine.
Date: May 16, 1949
Creator: Carpenter, D. E.; Johnston, C. P. & Susano, C. D.
System: The UNT Digital Library
Preparation of Ductile Zirconium: Summary of Thermodynamic Data (open access)

Preparation of Ductile Zirconium: Summary of Thermodynamic Data

Abstract: A summary of thermodynamic calculations for zirconium halides is given. Data indicates that the iodide is the most promising of the halides for arc dissociation and that good recoveries of zirconium should be obtainable provided dissociation is carried out at reduced pressure.
Date: September 16, 1949
Creator: Findlay, G. R.
System: The UNT Digital Library
Procedures in Magnetic Measurements at the University of California Radiation Laboratory, Berkeley:  Fields Which are Constant or Vary Slowly with Time (open access)

Procedures in Magnetic Measurements at the University of California Radiation Laboratory, Berkeley: Fields Which are Constant or Vary Slowly with Time

The flux standard is a device which will give a known flux-linkage change to be used as a calibration. At the Radiation Laboratory, two types of flux standards are used, a stationary type and a portable type.
Date: August 16, 1949
Creator: Richardson, Robert E.
System: The UNT Digital Library
Altitude-wind-tunnel investigation of various can-type burners in Bumblebee 18-inch ram jet (open access)

Altitude-wind-tunnel investigation of various can-type burners in Bumblebee 18-inch ram jet

An investigation on various can-type burners in a Bumblebee 18-inch ram jet under controlled conditions of pressure altitude and ram pressure ratio was conducted in the NACA Lewis altitude wind tunnel with kerosene as fuel. The performance of the following can-type burner configurations was better than that of the other burner configurations investigated: (1) a flame holder having a two-pitch alinement of perforations, 0.07-inch-wide cooling slots, and an arrangement of fuel nozzles located within an annulus having a mean radius of 7.24 inches; and (2) a flame holder having a zero-pitch alinement of perforations, 0.16-inch-wide cooling slots, and an annulus of fuel nozzles having a mean radius of 6.89 inches.
Date: March 16, 1949
Creator: Dupree, D. T.; Nussdorfer, T. J. & Sterbentz, W. H.
System: The UNT Digital Library
An NACA Vane-Type Angle-of-Attack Indicator for use at Subsonic and Supersonic Speeds (open access)

An NACA Vane-Type Angle-of-Attack Indicator for use at Subsonic and Supersonic Speeds

A vane-type angle-of-attack indicator suitable for measurements at both subsonic and supersonic speeds has been developed by the National Advisory Committee for Aeronautics. A brief history is given of the development, and a wind-tunnel calibration of the indicator is presented, together with a discussion of the corrections to be applied to the indicated readings.
Date: August 16, 1949
Creator: Mitchell, Jesse L. & Peck, Robert F.
System: The UNT Digital Library
On Reflection of Shock Waves from Boundary Layers (open access)

On Reflection of Shock Waves from Boundary Layers

Measurements are presented at Mach numbers from about 1.3 to 1.5 of reflection characteristics and the relative upstream influence of shock waves impinging on a flat surface with both laminar and turbulent boundary layers. The difference between impulse and step waves is discussed and their interaction with the boundary layer is compared. General considerations on the experimental production of shock waves from wedges and cones and examples of reflection of shock waves from supersonic shear layers are also presented.
Date: August 16, 1949
Creator: Liepmann, H. W.; Roshko, A. & Dhawan, S.
System: The UNT Digital Library