The Chemistry of Uranium(VI) Orthophosphate Solutions. Part 2. The Solubility of Uranium(VI) Orthophosphates in Phosphoric Acid Solutions (open access)

The Chemistry of Uranium(VI) Orthophosphate Solutions. Part 2. The Solubility of Uranium(VI) Orthophosphates in Phosphoric Acid Solutions

This report is about The Chemistry of Uranium(VI) Orthophosphate Solutions. a series of reports describing an investigation of the Uranium(VI) Orthophosphate system.
Date: June 30, 1953
Creator: Schreyer, J .M. & Baes, C. F., Jr.
Object Type: Report
System: The UNT Digital Library
COUNTERCURRENT ION EXCHANGE. FINAL SUMMARY REPORT. Report No. 34 (open access)

COUNTERCURRENT ION EXCHANGE. FINAL SUMMARY REPORT. Report No. 34

None
Date: June 30, 1953
Creator: Hiester, N.K. & Phillips, R.C.
Object Type: Report
System: The UNT Digital Library
Design Study for a 15-BeV Accelerator (open access)

Design Study for a 15-BeV Accelerator

This report is the culmination of a year of progress and planning in the high-energy particle field. During this year the Brookhaven Cosmotron has been successfully completed and brought into operation for research at 2.3 Bev. Preliminary experimental results with the copious output of π-mesons are in process of publication. Multiple production of mesons has been observed, a few V-particles detected, and the interactions of π-mesons in hydrogen have been studied. Yet it already appears that higher energies will be needed to produce and study the several new heavy particles detected in cosmic ray observations.
Date: June 30, 1953
Creator: Livingston, M., Stanley, Prof.; Ramsey, N. F., Prof.; Street, J. C., Prof.; Pound, R. V., Prof; Preston, W. M., Prof; Selove, W., Prof. et al.
Object Type: Report
System: The UNT Digital Library
DETERMINATION OF RARE EARTHS IN REFINED URANIUM (open access)

DETERMINATION OF RARE EARTHS IN REFINED URANIUM

None
Date: June 30, 1953
Creator: Ewing, R. A. & Bearse, A. E.
Object Type: Report
System: The UNT Digital Library
Determination of Rare Earths in Refined Uranium : Topical Report (open access)

Determination of Rare Earths in Refined Uranium : Topical Report

Abstract: "Rare-earth analyses were performed on several samples of refined uranium oxide and nitrate, using a modified cellulose column procedure. Rare earths were not detectable in samples of 0.03 shotgun of less. Detection limits were from 0.0005 to 0.015 ppm. Negligible quantities of low-cross-section rare earths were found in less pure uranium samples, obtained during start-up operations of the pilot plant at the Feed Materials Production Center, primarily those rare earths of greater than average abundance in nature. No correlation was found between rare-earth content and shotgun values. Rare earths do not appear to be contributing significantly to the neutron absorption of refined uranium. A modified cellulose column procedure, which includes a preconcentration solvent-extraction step, is described. Radioactive tracer tests indicating rare-earth recoveries by the method of >98 per cent are reported."
Date: June 30, 1953
Creator: Ewing, R. A. & Bearse, A. E.
Object Type: Report
System: The UNT Digital Library
An Exploratory Investigation of Some Types of Aeroelastic Instability of Open and Closed Bodies of Revolution Mounted on Slender Struts (open access)

An Exploratory Investigation of Some Types of Aeroelastic Instability of Open and Closed Bodies of Revolution Mounted on Slender Struts

"Aeroelastic instability phenomena of isolated open and closed rigid bodies of revolution free to move under elastic restraint have been investigated experimentally at low speeds by means of models suspended at zero angles of attack and yaw on slender flexible struts from a wind tunnel ceiling. Three types of instability were observed - flutter similar to classical bending-torsion flutter, divergence, and an uncoupled oscillatory instability which consists in nonviolent continuous or intermittent small-amplitude oscillations involving only angular deformations. The speeds at which this oscillatory instability starts were found to be as low as about one-third of the speed at flutter or divergence and to depend on the shape of the body, particularly that of the afterbody, and on the relative location of the elastic axis" (p. 1).
Date: June 30, 1953
Creator: Clevenson, S. A.; Wildmayer, E., Jr. & Diederich, Franklin W.
Object Type: Report
System: The UNT Digital Library
Investigation of a Half-Conical Scoop Inlet Mounted at Five Alternate Circumferential Locations Around a Circular Fuselage: Pressure-Recovery Results at a Mach Number 2.01 (open access)

Investigation of a Half-Conical Scoop Inlet Mounted at Five Alternate Circumferential Locations Around a Circular Fuselage: Pressure-Recovery Results at a Mach Number 2.01

The effects of inlet circumferential position around the fuselage on the characteristics of a half-conical scoop inlet having a 24.6deg half-angle cone have been investigated in the langley 4- by 4-foot supersonic pressure tunnel. Pressure-recovery results have been obtained at a Mach number of 2.01 for a fixed boundary-layer-bleed height which was 60 percent of the boundary-layer thickness at an angle of attack of 0deg, and for cowling position parameters of 42.4deg and 38.0deg. inlet had a capture area equal to 24.9 percent of the basic-fuselage frontal area. The angle of attack was varied from 0deg to 12deg.
Date: June 30, 1953
Creator: Hasel, Lowell E.; Lankford, John L. & Robins, A. W.
Object Type: Report
System: The UNT Digital Library
Preliminary flight measurements of the dynamic longitudinal stability characteristics of the Convair XF-92A delta-wing airplane (open access)

Preliminary flight measurements of the dynamic longitudinal stability characteristics of the Convair XF-92A delta-wing airplane

Report presenting an analysis of some longitudinal maneuvers obtained during performance tests of the Convair XF-92A by using measured period and time to damp to half amplitude and with a computer to give a preliminary measurement of the airplane stability and damping at a range of Mach numbers. Results indicated that no loss in control effectiveness was shown, the static stability increased with Mach number, the damping was light but positive, and the damping factor was low.
Date: June 30, 1953
Creator: Holleman, Euclid C.; Evans, John H. & Triplett, William C.
Object Type: Report
System: The UNT Digital Library
Progress Report - Studies on the Propagation of Gamma Rays in Air (open access)

Progress Report - Studies on the Propagation of Gamma Rays in Air

Initial rough measurements of the quality of the gamma radiation from Co-60 in air indicated agreement with the theoretical calculations of Spencer and Fano for an infinite water medium. Further experiments were performed, duplicating the conditions assumed in the calculations. Since the spectral region between 100 kev and 1 mev has already been examined by Hayward, it was decided to investigate in detail the region below 100 kev and above 1.0 mev. Total radiation dosage measurements were made in water using Victoreen ion chambers. The build-up factor was measured as a function of distance. Good agreement was obtained with the results of White. The spectrum below 150 kev was examined with a small NaI(Tl) scintillation counter and both the shape of the spectrum and the attenuation as a function of distance was in good agreement with the calculations. At distance less than 30 cm from the source the spectral shape changed, gradually broadening with the peak shifting to higher energies. The primary region above 1.0 mev was examined using a large NaI(Tl) crystal, and the gradual loss of resolution in the two primaries as a function of distance with an increase in lower energy events was shown. The measurements to …
Date: June 30, 1953
Creator: Bernstein, W. & Weiss, M. M.
Object Type: Report
System: The UNT Digital Library
Recent Developments in Powder Metallurgy (open access)

Recent Developments in Powder Metallurgy

Brief notes from a meeting between NAA and S. B. Roboff, Sylvania Electric Products, regarding the important developments in powder metallurgy fuels and reactor materials.
Date: June 30, 1953
Creator: Hayward, B.R.
Object Type: Report
System: The UNT Digital Library
Removal of Graphite from Aluminum Surfaces (open access)

Removal of Graphite from Aluminum Surfaces

The first of two general methods are discussed based on the removal of the thin layer of aluminum to which graphite adheres. Two electro-polishing techniques, an electrolytic etch, an anodization-deanodication cycle and two chemical etches are described.
Date: June 30, 1953
Creator: Dillon, R. L. & Hodgson, W. H.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-61 (open access)

Texas Attorney General Opinion: S-61

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: Legality of a District Attorney receiving a 10% commission on collections on an account due for board and treatment when payments are to be made in monthly installments under submitted contracts.
Date: June 30, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: taper-ratio series (open access)

Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: taper-ratio series

Report presenting a continuation of the program in the high-speed 7- by 10-foot tunnel to investigate the aerodynamic characteristics in pitch, sideslip, and steady roll of model configurations with variations in wing geometric parameters. This report contains the aerodynamic characteristics in pitch of wing-fuselage combinations with wings of aspect ratio 4, sweepback angle of 45 degrees, and three different taper ratios. Results regarding lift characteristics, pitching-moment characteristics, drag characteristics, and lift-drag ratio are provided.
Date: June 30, 1953
Creator: King, Thomas J., Jr. & Pasteur, Thomas B., Jr.
Object Type: Report
System: The UNT Digital Library
Analytical study of blockage- and lift-interference corrections for slotted tunnels obtained by the substitution of an equivalent homogeneous boundary for the discrete slots (open access)

Analytical study of blockage- and lift-interference corrections for slotted tunnels obtained by the substitution of an equivalent homogeneous boundary for the discrete slots

From Introduction: "This paper will treat the problem in the suggested manner, beginning with the development of a suitable boundary condition to represent mathematically a homogeneous boundary which has the same flow characteristics, at a point in the flow sufficiently removed from the boundary as the actual physical boundary of alternate open and closed portions of the wall. Numerical results will be presented for circular tunnels with uniformly distributed around the circumference, for rectangular tunnels with uniformly distributed around the circumference, for rectangular tunnels with uniformly distributed slots in the top and bottom walls, for rectangular tunnels with the slot distribution determined by a transformation from a uniformly slotted circular tunnel, and for a two-dimensional tunnel. The results of this paper are derived on the basis of an incompressible potential flow."
Date: June 29, 1953
Creator: Davis, Don D., Jr. & Moore, Dewey
Object Type: Report
System: The UNT Digital Library
A comparison of gust loads measured in flight on a swept-wing airplane and an unswept-wing airplane (open access)

A comparison of gust loads measured in flight on a swept-wing airplane and an unswept-wing airplane

Report presenting flight testing with two jet-propelled airplanes in rough air to investigate effects of sweep on gust loads and gust selectivity. Data was taken with an unswept-wing airplane and a 35 degree swept-wing airplane for incremental accelerations corresponding to airspeeds of 300 and 450 miles per hour. The results indicated that the swept-wing airplane experienced lower loads in turbulent air than the unswept-wing airplane.
Date: June 29, 1953
Creator: Funk, Jack & Mickleboro, Harry C.
Object Type: Report
System: The UNT Digital Library
Electron Loading and High Voltage Sparking of Metals in Vacuum (open access)

Electron Loading and High Voltage Sparking of Metals in Vacuum

Statistical methods were employed to measure relative values of electron loading and spark-over voltage for a large number of unoutgassed electrode materials. Test voltages up to 110 KV were employed in vacuum of the order of 10<sup>-7 mm Hg. All metals showed a square root dependence between spark-over voltage and spacing.
Date: June 29, 1953
Creator: Heard, Harry G.
Object Type: Report
System: The UNT Digital Library
Flight-Determined Pressure Distributions Over the Wing of the Bell X-1 Research Airplane (10-Percent-Thick Wing) at Subsonic and Transonic Speeds (open access)

Flight-Determined Pressure Distributions Over the Wing of the Bell X-1 Research Airplane (10-Percent-Thick Wing) at Subsonic and Transonic Speeds

Report presenting measurements of chordwise pressure distributions at four spanwise stations over a 10-percent-thick wing of the Bell X-1 airplane. Results regarding pressure distributions at the various stations and section aerodynamic characteristics are presented. The data was obtained for a range of Mach numbers from 0.30 to 11.9 and altitudes from 17,000 to 47,000 with several different types of maneuvers.
Date: June 29, 1953
Creator: Knapp, Ronald J. & Jordan, Gareth H.
Object Type: Report
System: The UNT Digital Library
Investigation at Low Speed of the Flow Field Behind the Lifting Surfaces of a Model Equipped With a 60 Degree Triangular Wing and a 60 Degree Triangular Canard Tail (open access)

Investigation at Low Speed of the Flow Field Behind the Lifting Surfaces of a Model Equipped With a 60 Degree Triangular Wing and a 60 Degree Triangular Canard Tail

Report presenting an investigation of the flow behind the lifting surfaces of a model equipped with a 60 degree triangular wing and a 60 degree triangular canard tail. Results regarding the force and moment data, air-stream surveys behind the wing, effective values of downwash and dynamic-pressure ratio, effect of tail height and length, a comparison with previous data, the effects of component area and ratio, and the effect of a canard tail are provided.
Date: June 29, 1953
Creator: Newman, Ernest E. & Cahill, Jones F.
Object Type: Report
System: The UNT Digital Library
Performance of a Normal-Shock Scoop Inlet with Boundary-Layer Control (open access)

Performance of a Normal-Shock Scoop Inlet with Boundary-Layer Control

Memorandum presenting tests made on a normal-shock inlet mounted as a scoop on a flat plate on which a turbulent boundary layer was generated. A boundary-layer-removal scoop was provided between the inlet and the plate and various amounts of the boundary layer were removed. Results regarding the main inlet, boundary-layer scoop, and an evaluation of results are provided.
Date: June 29, 1953
Creator: Frazer, Alson C. & Anderson, Warren E.
Object Type: Report
System: The UNT Digital Library
A Problem in the Conversion of Neutron Dose to Flux (open access)

A Problem in the Conversion of Neutron Dose to Flux

This report discusses the calculation involved in converting neutron dose to flux. In order to test conversion calculation methods, the flux entering the Oak Ridge National Laboratory Lid Tank and the water by the north face of the Oak Ridge National Laboratory Bulk Shielding Reactor was used.
Date: June 29, 1953
Creator: McMillan, D. E.
Object Type: Report
System: The UNT Digital Library
Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method (open access)

Procedure for Measuring Liquid-Water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method

"The rotating multicylinder method for in-flight determination of liquid-water content, droplet size, and droplet-size distribution in icing clouds is described. The theory of operation, the apparatus required, the technique of obtaining data in flight, and detailed methods of calculating the results, including necessary charts and tables, are presented" (p. 1).
Date: June 29, 1953
Creator: Lewis, William; Perkins, Porter J. & Brun, Rinaldo J.
Object Type: Report
System: The UNT Digital Library
Spectrographic Analysis of Plutonium by the Thenoyltrifloroacetone Extraction Method (open access)

Spectrographic Analysis of Plutonium by the Thenoyltrifloroacetone Extraction Method

Impurities are separated from plutonium solutions by means of TTA (thenoyltrifluoracetone) extractions. Plutonium in hydrochloric acid solution is reduced to the trivalent state with hydroxylamine, and some impurities are extracted into hezone or a solution of TTA in hezone. The organic phase is removed, and the plutonium in the aqueous phase is oxidized to the tetravalent state with nitric acid. Investigations of several variables which affect the extraction are described..
Date: June 29, 1953
Creator: Van Tuyl, H. H.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-58 (open access)

Texas Attorney General Opinion: S-58

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: Authority of Teacher Retirement System to pool all assets of all funds of the System for investment purposes.
Date: June 29, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-59 (open access)

Texas Attorney General Opinion: S-59

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: Authority of the judge of the new special probate court in Galveston County to act on delayed registrations of births and deaths.
Date: June 29, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History