Resource Type

100 Areas, January 15 through January 21 (open access)

100 Areas, January 15 through January 21

This report gives the weekly progress for the B, D, and F piles. The report also gives a brief discussion of the following activities: process water control and pressure drop studies; purging of D, B, and F piles; slug corrosion studies; tube corrosion studies; thimble corrosion studies; and graphite expansion studies.
Date: January 25, 1946
Creator: Jordan, W. E.
System: The UNT Digital Library
100 Areas technical activities report: Engineering, June 1947 (open access)

100 Areas technical activities report: Engineering, June 1947

There were no cases of unusual blistering of slugs being followed under Production Tests. Two normal production tubes were borescoped following trouble with discharge. In Tube 3188-D a distorted slug became stuck in the region of sharp curvature near the inner end of the rear gun barrel; this is the first time this phenomenon has occurred. Examination of irradiated slugs of rolled metal after normal exposure indicates that rolled material has no particular advantages over extruded material from the standpoint of blistering. However, no extensively blistered pieces were found in either the rolled metal are being held for more extended exposure. Inspection of a large number of Van Stone flanges in the D and F Piles has confirmed that the inlet flanges are in generally good condition but that the rear Van Stone flanges of tubes in the 0.140-inch orifice sone of both piles were badly corroded and generally contained deep pits that extended about half-way through the flange. The Van Stone test units are to be installed unshielded in the risor room at the rear of the D Pile, since the shielding required in the X Sample Room exceeded the allowable floor loading. Recent experimental observations indicate that solid …
Date: June 25, 1947
Creator: Woods, W. K.
System: The UNT Digital Library
300 Area, January 15--January 21 (open access)

300 Area, January 15--January 21

This report from the reactor fuel manufacturing facilities at Hanford highlights extrusion, canning, and welding operations. Processing of thorium and bismuth is discussed. Radiography of fuels revealed voids that conformed underweight reject measurements.
Date: January 25, 1946
Creator: Kidder, C. P.
System: The UNT Digital Library
Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336 (open access)

Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336

A 1/5.5-size powered dynamic model of the Columbia XJL-1 amphibian was landed in Langley tank no. 1 in smooth water and in oncoming waves of heights from 2.1 feet to 6.4 feet (full-size) and lengths from 50 feet to 264 feet (full-size). The motions and the vertical accelerations of the model were continuously recorded. The greatest vertical acceleration measured during the smooth-water landings was 3.1g.
Date: September 25, 1947
Creator: Clement, Eugene P. & Havens, Robert F.
System: The UNT Digital Library
Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance (open access)

Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance

"Investigations were conducted in the Cleveland altitude wind tunnel to determine the performance and operational characteristics of the 19B-2, 19B-8, and 19XS-1 turbojet engines. One objective was to determine the effect of altitude, flight Mach number, and tail-pipe-nozzle area on the performance characteristics of the six-stage and ten-stage axial-flow compressors of the 19B-8 and 19XB-1 engines, respectively, The data were obtained over a range of simulated altitudes and flight Mach numbers" (p. 1).
Date: April 25, 1947
Creator: Dietz, Robert O. & Kuenzig, John K.
System: The UNT Digital Library
Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine 1: Performance with tail-pipe burning (open access)

Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine 1: Performance with tail-pipe burning

From Introduction: "Performance results of the tail-pipe burning investigation on the TG-180 turbojet engine and a comparison of experimental results with theoretical calculations are presented."
Date: September 25, 1946
Creator: Fleming, W. A. & Dietz, R. O.
System: The UNT Digital Library
An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane (open access)

An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane

From Introduction: "This report presents an analysis based on flight and wind-tunnel test data directed toward the determination of the probable cause of the pitch-up. Wing pressure distribution and stability and control characteristics in the dive are also included."
Date: September 25, 1947
Creator: Brown, Harvey H.; Rolls, L. Stewart & Clousing, Lawrence A.
System: The UNT Digital Library
Annual Report of the Boy Scouts of America: 1942 (open access)

Annual Report of the Boy Scouts of America: 1942

Annual report submitted by the Boy Scouts of America to Congress describing highlights from 1942, activities, service reports, honors, finance, organizational leadership, and other information about scouting programs.
Date: March 25, 1943
Creator: Boy Scouts of America
System: The Portal to Texas History
ATTEMPTS TO PREPARE TRIFLUOROACETIC ACID BY THE REACTION OF COBALTIC FLUORIDES WITH ACETIC ANHYDRIDE AND ACETONITRILE (open access)

ATTEMPTS TO PREPARE TRIFLUOROACETIC ACID BY THE REACTION OF COBALTIC FLUORIDES WITH ACETIC ANHYDRIDE AND ACETONITRILE

None
Date: May 25, 1945
Creator: Halbedel, H.S.
System: The UNT Digital Library
Calculations for Some Pile Shapes of Which the Boundaries are Partly Spherical (open access)

Calculations for Some Pile Shapes of Which the Boundaries are Partly Spherical

Some methods for calculating the k requirements of various shaped piles are indicated, with particular reference to the shape of the tank in the homogeneous plant.
Date: February 25, 1944
Creator: Young, G.; Murray, F. H. & Castle, H.
System: The UNT Digital Library
Chemical Properties of Uranium Hexafluoride, UF6 (open access)

Chemical Properties of Uranium Hexafluoride, UF6

Uranium hexafluoride has the distinction of being the only stable gaseous compound of uranium known up to the present moment. Because of this property it is the only compound that can be used for processes of isotope separation, such as diffusion, thermal diffusion, centrifuge separation, distillation, and other of a similar nature. Here is a short description of the properties of UF{sub 6} and is intended for a reader interested only casually in this compound. UF{sub 6} is a very reactive compound and a very strong fluorinating agent. It is immediately hydrolized by water. In fluorinating reactions it is reduced to the green highly stable UF{sub 4}. It reacts instantaneously with hydrogen at room temperature. It fluorinates many metals; sodium and mercury are attacked in the cold, lead, zinc, tin and iron on heating; platinum and gold react only above 400 C. With organic compounds like alcohol, ether, benzene or toluene, immediate fluorination takes place with formation of HF and carbon or carbonaceous material. The compound forms colorless, very volatile, beautiful transparent crystals of high refractive index. Melting point = 69.5{sup o}; boiling point at 760 mm = 56.2{sup o}; D20{sup o} = 4.68. The crystals melt water pressure to …
Date: June 25, 1941
Creator: Grosse, Aristid V.
System: The UNT Digital Library
Corrosion Tests on Tantalum, Hastelloy C and Duriron in 234-5 Project Solutions (open access)

Corrosion Tests on Tantalum, Hastelloy C and Duriron in 234-5 Project Solutions

Introduction: "Room temperature and elevated temperature, static immersion and vapor suspicion, corrosion tests were conducted with Duriron, Hastelloy C, and tantalum in hydriotic acid and 234-5 project process supernatant solution (synthetic environments. The data relevant to these tests are contained herein."
Date: February 25, 1949
Creator: Work, J. B. & Koenig, W. W.
System: The UNT Digital Library
CRITICAL DIMENSIONS OF UNTAMPED CONICAL VESSELS (open access)

CRITICAL DIMENSIONS OF UNTAMPED CONICAL VESSELS

None
Date: August 25, 1947
Creator: Murray, R.
System: The UNT Digital Library
Critical Dimensions of Untamped Conical Vessels (open access)

Critical Dimensions of Untamped Conical Vessels

Abstract: "The need often arises for determining the critical chemical concentration of uranium solution in the conical bottom of a plant reactor or storage vessel, or the dimension if the concentration is known. This report describes the mathematical analysis of Poisson's equation for a spherical sector, which approximates a right circular cone. The ratio of the critical dimension of an equivalent sphere to the height of the sector for various sector angles is derived from a comparison of first eigenvalues. No description of further relations between composition and dimensions is discussed in the report."
Date: August 25, 1947
Creator: Murray, Raymond
System: The UNT Digital Library
Density of Solid Hex Uf$Sub 6$ Near the Triple Point, and the Expansivity of the Liquid From the Triple Point to 92 C (open access)

Density of Solid Hex Uf$Sub 6$ Near the Triple Point, and the Expansivity of the Liquid From the Triple Point to 92 C

The report addresses the density of solid hex near the Triple and the expansivity of the liquid from the triple point.
Date: February 25, 1943
Creator: Wechsler, Martin T. & Hoge, Harold J.
System: The UNT Digital Library
Determination of reactivity coefficients and rod calibration of D Pile. Interim report on Production Test No. 105-97-P (open access)

Determination of reactivity coefficients and rod calibration of D Pile. Interim report on Production Test No. 105-97-P

The test of March 7, 1947 was planned as a check on power coefficient values; however, an analysis of reactivity data gave evidence of a considerable flattening of ``A`` rod in the region between 0--75 inches out. A second test of longer duration was therefore made on April 1, 1947 in order to obtain a check calibration of this portion of the control rod. The results of this test verified the flattening of this portion of ``A`` rod. The redetermined power coefficients based on new rod calibrations are given.
Date: April 25, 1947
Creator: Kruesi, F. E.
System: The UNT Digital Library
Determination of Stress-Rupture Parameters for Four Heat-Resisting Alloys (open access)

Determination of Stress-Rupture Parameters for Four Heat-Resisting Alloys

Stress-rupture data for four heat-resisting alloys are analyzed according to equations of the theory of rate processes. A method for determining the four parameters of structure and composition is demonstrated and the four parameters are determined for each of the alloys: forged S816, cast S816, cast S590, and cast Vitallium. It is concluded that parameters can be determined for an alloy provided sufficient reliable experimental data are available.
Date: August 25, 1947
Creator: Lidman, William G.
System: The UNT Digital Library
Determination of Tuballoy Uranium With the X-Ray Spectrograph. Summary Report (open access)

Determination of Tuballoy Uranium With the X-Ray Spectrograph. Summary Report

None
Date: October 25, 1945
Creator: unknown
System: The UNT Digital Library
Developments in the Casting Department of the Metal Production Plant at Iowa State College. Special Report on the Casting of Uranium at Iowa State College (open access)

Developments in the Casting Department of the Metal Production Plant at Iowa State College. Special Report on the Casting of Uranium at Iowa State College

This report addresses the casting of uranium rods at iowa state college.
Date: August 25, 1945
Creator: Wilhelm, H. A.
System: The UNT Digital Library
Direct Conversion of the TF₆ to TCl₄ (open access)

Direct Conversion of the TF₆ to TCl₄

The following report provides a general summary of some methods that could be used to convert hexafluoride into tetrafluoride, but is mainly devoted to the work done on the conversion of tetrafluoride to tetrachloride.
Date: September 25, 1945
Creator: Calkins, Vincent P.
System: The UNT Digital Library
Direct Current Electromagnetic Pumps (open access)

Direct Current Electromagnetic Pumps

Abstract: "A number of direct current conduction type electromagnetic pumps for liquid metals were constructed. Pumping capacities of over 400 gpm and efficiencies of over 50 percent were obtained. NaK alloy at temperatures up to 400 C was used in the test. The large currents required were obtained from rectifiers or from a homopolar generator constructed for the purpose."
Date: October 25, 1949
Creator: Barnes, A. H.; Smith, F. A. & Whitham, G. K.
System: The UNT Digital Library
Eastern Black Shale Reconnaissance Preliminary Report (open access)

Eastern Black Shale Reconnaissance Preliminary Report

The following report is the result of a reconnaissance of the black shales of the Eastern United States in the summer of 1944. The purpose of this reconnaissance was to determine the radioactivity of the shales, specifically for uranium and thorium.
Date: August 25, 1944
Creator: Slaughter, A. L. & Clabaugh, S. E.
System: The UNT Digital Library
The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65 (open access)

The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65

The results of an investigation of two 10-foot-diameter, two-blade NACA propellers are presented for a range of blade angles from 20 degrees to 55 degrees at airspeeds up to 500 miles per hour. These results are compared with those from previous investigations of five related NACA propellers in order to evaluate the effects of blade-section thickness ratios on propeller aerodynamic characteristics.
Date: April 25, 1949
Creator: Maynard, Julian D. & Steinberg, Seymour
System: The UNT Digital Library
Effect of Normal Pressure on the Critical Compressive Stress of Curved Sheet (open access)

Effect of Normal Pressure on the Critical Compressive Stress of Curved Sheet

Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress. (author).
Date: August 25, 1942
Creator: Rafel, Norman
System: The UNT Digital Library