Chemical Development Status Report for Week Ending May 25, 1956 (open access)

Chemical Development Status Report for Week Ending May 25, 1956

None
Date: June 7, 1956
Creator: Blanco, R. E. & Ferguson, D. E.
System: The UNT Digital Library
The Results of the D-12 Boil Up Test and Recommendations to Improve the Performance of Bayonet Tube Bundles (open access)

The Results of the D-12 Boil Up Test and Recommendations to Improve the Performance of Bayonet Tube Bundles

The purpose of this report is to describe the tests performed on the D-12 waste evaporator, to present and evaluate the data obtained during the test, and to make recommendations for the implementation and operation of present and future installations of bayonet tube bundles.
Date: February 7, 1956
Creator: Cook, M. W.
System: The UNT Digital Library
Analysis of High Purity Water by Spectrochemistry (open access)

Analysis of High Purity Water by Spectrochemistry

When water is used as a coolant in any heat-producing process, the purity of the cooling water is of considerable importance, both from the standpoint of build-up of deposited solids inside the cooling tubes, and as an indication of corrosion of the tubes or any other materials with which the water comes in contact. The first problem has long been recognized, and is generally solved by pretreatment of the water. Efficient treatment can reduce the total solids content to less than 0.1 ppm, and the concentration of individual elements to the order of 0.01 ppm. If water of this purity is used, the analysis of the input and output stresses can result in some useful information. The input stream analysis, of course, is direct measure of the quality of the original cooling water, and frequent analysis by a reasonably fast method can be used to keep pretreatment under control. But of even greater significance is the difference in the impurity content of input and output streams. In a simple, straight-through system the difference generally will be negligible. If a closed, recirculating system is considered, however, with the coolant water circulating through the process to be cooled and then through a …
Date: May 7, 1956
Creator: Daniel, J. L. & Ko, R.
System: The UNT Digital Library
Radiobiological Studies of the Columbia River Through December, 1955 (open access)

Radiobiological Studies of the Columbia River Through December, 1955

Radiobiological studies were made to determine effects of radioactive effluents from the Hanford reactors upon the aquatic biota of the Columbia River and to evaluate related hazards. Data from studies completed between September, 1945, and December, 1955 are presented and interpreted. All forms of life were many times more radioactive than the water they inhabited. Some radioisotopes were much more readily accumulated than others in living organisms. Differences in the concentration of certain radioisotopes by various species of organisms and kinds of body tissue are described; and geographical, seasonal and annual fluctuations in the concentration of radioisotopes in organisms are discussed.
Date: November 7, 1956
Creator: Davis, J. J.; Watson, D. G. & Palmiter, C.C.
System: The UNT Digital Library
Hanford Test Pile (open access)

Hanford Test Pile

The Hanford Test Pile is a heterogeneous, low power, graphite moderated natural uranium pile. The pile consists of an eighteen foot cube of graphite containing 292 charged channels in a square array with an 8-1/2-inch lattice spacing. This report describes the reactor and the operating procedures used, and presents the latest results of calibrations performed. These calibrations supersede other work which has been done on the Test Pile and contain refinements of most of the early calibrations.
Date: June 7, 1956
Creator: Davis, M. V. & Fowler, H. A.
System: The UNT Digital Library
Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102B Airplane at Mach Numbers of 1.41, 1.61, and 2.01: Coord No. AF-231 (open access)

Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102B Airplane at Mach Numbers of 1.41, 1.61, and 2.01: Coord No. AF-231

Report discussing testing of a scale model of the Convair F-102B to determine its aerodynamic characteristics at several Mach numbers. Four basic body modifications and two afterbody configurations were evaluated.The body modifications were all found to slightly reduce values of minimum drag, but did not cause a change in the static stability and lift-curve-slope values compared to the F-102A.
Date: February 7, 1956
Creator: Driver, Cornelius & Robinson, Ross B.
System: The UNT Digital Library
Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications (open access)

Data From Large-Scale Low-Speed Tests of Airplane Configurations With a Thin 45 Degree Swept-Wing Incorporating Several Leading-Edge Contour Modifications

Memorandum presenting force tests that have been made of airplane configurations with a thin swept wing incorporating several wing-contour modifications forward of maximum thickness. Both longitudinal and lateral characteristics are provided.
Date: May 7, 1956
Creator: Evans, William T.
System: The UNT Digital Library
Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels (open access)

Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels

An investigation of the effect of extremely high altitude operation on the performance and operating characteristics of two turbojet engines using gaseous hydrogen and JP-4 fuels. At extremely high altitude conditions, engine performance was significantly poorer than at low altitudes. The majority of performance losses were due to the compressor because of low Reynolds number and the combustor because of low combustion efficiency.
Date: August 7, 1956
Creator: Fleming, W. A.; Kaufman, H. R.; Harp, J. L., Jr. & Chelko, L. J.
System: The UNT Digital Library
Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels (open access)

Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels

Two current turbojet engines were operated with gaseous-hydrogen and JP-4 fuels at very high altitudes and a simulated Mach number of 0.8. With gaseous hydrogen as the fuel stable operation was obtained at altitudes up to the facility limit of about 90,000 feet and the specific fuel consumption was only 40 percent of that with JP-4 fuel. With JP-4 as the fuel combustion was unstable at altitudes above 60,000 to 65,000 feet and blowout limits were reached at 75,000 to 80,000 feet. Over-all performance, component efficiencies, and operating range were reduced considerable at very high altitudes with both fuels.
Date: August 7, 1956
Creator: Fleming, W. A.; Kaufman, H. R.; Harp, J. L., Jr. & Chelko, L. J.
System: The UNT Digital Library
Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces (open access)

Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

Report presenting a free-flight investigation to determine the effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a configuration with 52.5 degrees sweptback wing of aspect ratio 3, and inline tail surfaces. Results regarding drag, total normal force and pitching moment, and wash at the horizontal tail are provided.
Date: May 7, 1956
Creator: Gillespie, Warren, Jr.
System: The UNT Digital Library
Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71 (open access)

Minimum Drag of Four Versions of a Swept-Wing Fighter Airplane Obtained From Flight Tests of Rocket-Boosted Models at Mach Numbers From 0.81 to 1.71

Memorandum presenting tests conducted with four specific versions of a swept-wing fighter airplane, which indicate that a large reduction in external-drag coefficient was accomplished by redesigning the original configuration. The forebody modifications, which consisted of a smaller canopy, slimmer nose, and sharper inlet lip, reduced the value of the external-drag coefficient from 0.044 to 0.042 at a Mach number of 1.05 and from 0.042 to 0.040 at a Mach number of 1.28.
Date: September 7, 1956
Creator: Hastings, Earl C., Jr.
System: The UNT Digital Library
An Evaluation of the Corrosion and Oxidation Resistance of High-Temperature Brazing Alloys (open access)

An Evaluation of the Corrosion and Oxidation Resistance of High-Temperature Brazing Alloys

The fabrication of heat exchangers and radiators to be used in conjunction with high-temperature nuclear reactors may present exceedingly complex problems. Rigid heat transfer requirements may necessitate the use of compact assemblies of thin-walled small-diameter tubes as integral parts of the heat transfer units. Intricate designs may also be required in which cooling fins must be securely joined to the tubes at closely spaced intervals. In addition to the difficulties in fabrication imposed by the designs themselves, the high operating temperatures involved require the careful selection of materials and joining techniques. The choice of fabrication procedure for a given component must not only be based upon the stresses and temperatures to be encountered, but also upon special factors peculiar to nuclear service. Since many reactor applications employ highly corrosive environments, compatibility of the structural ma terials with the corrosive media is of paramount importance. The low nuclear cross-section require ment for brazing alloys to be used inside the re actor also places stringent limitations on the possible choices of in-pile applications. The use of boron in alloys for certain service may not be considered feasible, for example, because of its high nuclear absorption cross section. Although welding is used extensively …
Date: November 7, 1956
Creator: Hoffman, E. E.; Leitten, C. F., Jr.; Patriarca, P.; Slaughter, G. M.; Pope, J. E.; Shubert, C. E. et al.
System: The UNT Digital Library
A study of a missile designed to fly at low speed with its longitudinal axis aligned with the flight path (open access)

A study of a missile designed to fly at low speed with its longitudinal axis aligned with the flight path

An experimental investigation to explore the practicability of a low-speed missile designed to fly with its longitudinal axis pointing along the flight path. The wing and tail surfaces were arranged in a cruciform pattern and the incidence was selected to trim the missile at the desired normal-force coefficient with the body at 0 degrees angle of attack. Results regarding the description of a self-balancing missile and experimental results are provided.
Date: February 7, 1956
Creator: Hopkins, Edward J. & Sorensen, Norman E.
System: The UNT Digital Library
Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition (open access)

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition

Data were calculated for equivalence ratios of 1 to 3, chamber pressures of 300 and 600 pounds per square inch absolute, and pressure ratios of 1 to 1500. Parameters included are specific impulse, combustion and exit temperature, molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity. A correlation is given which permits determination of performance for a wide range of chamber pressures.
Date: September 7, 1956
Creator: Huff, Vearl N.; Fortini, Anthony & Gordon, Sanford
System: The UNT Digital Library
Examination of Irradiated Uranium-Magnesium Matrix Fuel Material (open access)

Examination of Irradiated Uranium-Magnesium Matrix Fuel Material

Twelve uranium-magnesium fuel material samples have been irradiated in the MTR at the request of the Pile metallurgy Unit. These samples were 0.40 inch in diameter by 1.5 inches long and were canned in Zircalloy-2 capsules. The uranium used in these specimens was in the form of chips which packs about 50 volume percent. Six of the samples contained a matrix of pure magnesium and the other six contained an alloy matrix of magnesium - 1.4 weight percent silicon. Two specimens of each matrix material were irradiated to 1000 MWD/T and a like number to 5000 MWD/T. Bend tests were performed on the samples and on unirradiated control samples to secure a measure of the effect of radiation exposure on the physical properties of the material.
Date: May 7, 1956
Creator: Kelly, W. S.
System: The UNT Digital Library
Nuclear Safety Consideration For Continuous Ion Exchange Column Design (open access)

Nuclear Safety Consideration For Continuous Ion Exchange Column Design

Considerable interest has been shown at HAPO in the development of a continuous ion exchange process for concentrating plutonium solutions. Development work has been performed on continuous ion exchange for both uranium and plutonium concentrations at the X-10 at ORNL. On a recent trip to Oak Ridge to discuss critical mass problems and experiments with Dr. A. D. Callihan of the ORNL critical mass facility, a meeting was also held with C. W. Hancher and R. Higgins of X-10 regarding continuous ion exchange operation. From this meeting, information was obtained that is helpful to work out nuclear safety aspects of such a plant for the concentration of plutonium solutions. An advance copy of "Countercurrent Ion Exchange" by T. A. Arehart, J. C. Bresee, C. W. Hancher, and S. H. Jury was obtained. This paper is to be presented at an AIChE meeting this fall. Preliminary blue prints of ORNL-3" Ion Exchange column design were also obtained. Upon my return to HAPO, a meeting was held with members of the Process Planning, Equipment Development, and Chemical Engineering Development Units of the Chemical Engineering Sub-Section (Separations Technology) to present the document and blue prints on continuous ion exchange and arrive at a …
Date: March 7, 1956
Creator: Ketzlach, N.
System: The UNT Digital Library
The storage and handling of J-slugs (open access)

The storage and handling of J-slugs

The nuclear safety specifications (1) for handling J-slugs have previously been reviewed. These specifications provided information for the storage of loaded 100-hole shipping containers and loaded 66-hole wood cart pallets in certain arrays. Storage of J-slugs in J-Material Crates conforming to Drawing No. H-3-6217 had not been reviewed for the previous specifications. It has become desirable to provide specifications for J-slug storage in these crates as well as make additions to the present specifications on the storage of these enriched slugs in shipping containers and pallets. The results of this study pertaining to arrays of J-slugs in shipping containers and pallets will be incorporated as an addition to the present specifications for handling J-slugs.
Date: February 7, 1956
Creator: Ketzlach, N.
System: The UNT Digital Library
Mechanical Features of a Continuous Ion Exchange Unit (open access)

Mechanical Features of a Continuous Ion Exchange Unit

This review covers: (a) The continuous countercurrent ion exchangers which have been described in the patent and/or technical literature. (b) Some of the other moving bed processes which are similar in mechanical arrangement to a continuous countercurrent ion exchange and which might have certain features adaptable to an ion exchange unit. (c) The auxiliary mechanical devices which are or may be used in an ion exchange apparatus.
Date: August 7, 1956
Creator: Lauer, B. E.
System: The UNT Digital Library
Survey of Refractory Uranium Compounds (open access)

Survey of Refractory Uranium Compounds

Abstract: Chemical and physical data on twenty binary uranium compounds that may prove suitable for refractory nuclear fuels were assembled. The compounds were those with aluminum, boron, carbon, iron, nickel, nitrogen, silicon, or sulfur. Too little is known at this time about the compounds to evaluate any of them for fuel. The program is being extended in an effort to provide the needed data.
Date: August 7, 1956
Creator: Loch, Luther D.; Engle, Glen B.; Snyder, M. Jack & Duckworth, Winston Howard
System: The UNT Digital Library
A simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed (open access)

A simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed

Report presenting a brief study utilizing pilots to fly a simulator of some longitudinal stability and control problems of an assumed aircraft capable of flights to altitudes essentially out of the atmosphere. The results show that more than the inherent longitudinal damping of the aircraft is necessary to affect a safe flight, particularly during entry into the atmosphere. Results regarding some preliminary considerations, entry, and control in ascent and the ballistics trajectory are provided.
Date: September 7, 1956
Creator: Matthews, Howard F. & Merrick, Robert B.
System: The UNT Digital Library
Torsional Stiffness of Thin-Walled Shells Having Reinforcing Cores and Rectangular, Triangular, or Diamond Cross Section (open access)

Torsional Stiffness of Thin-Walled Shells Having Reinforcing Cores and Rectangular, Triangular, or Diamond Cross Section

"A theoretical investigation has been made of the Saint-Venant torsion of certain composite bars. These bars are composed of two materials -- one material in the form of a thin-walled cylindrical shell and the other material in the form of a core which fills the interior of the shell and is bonded to it. An approximate boundary-value problem is formulated on assumptions similar to those of the theory of torsion of hollow thin-walled shells (Bredt theory)" (p. 771).
Date: June 7, 1956
Creator: McComb, Harvey G., Jr.
System: The UNT Digital Library
Wind-tunnel investigation of the damping in roll of the Douglas D-558-II research airplane and its components at supersonic speeds (open access)

Wind-tunnel investigation of the damping in roll of the Douglas D-558-II research airplane and its components at supersonic speeds

Experimental values of damping in roll at zero angle of attack of the Douglas D-558-II research airplane and its components have been obtained at five different Mach numbers. Large effects of Reynolds number, boundary layer, and wing-incidence angle on the damping in roll were obtained.
Date: September 7, 1956
Creator: McDearmon, Russell W.
System: The UNT Digital Library
Propagation of a free flame in a turbulent gas stream (open access)

Propagation of a free flame in a turbulent gas stream

Effective flame speeds of free turbulent flames were measured by photographic, ionization-gap, and photomultiplier-tube methods, and were found to have a statistical distribution attributed to the nature of the turbulent field. The effective turbulent flame speeds for the free flame were less than those previously measured for flames stabilized on nozzle burners, Bunsen burners, and bluff bodies. The statistical spread of the effective turbulent flame speeds was markedly wider in the lean and rich fuel-air-ratio regions, which might be attributed to the greater sensitivity of laminar flame speed to flame temperature in those regions. Values calculated from the turbulent free-flame-speed analysis proposed by Tucker apparently form upper limits for the statistical spread of free-flame-speed data. Hot-wire anemometer measurements of the longitudinal velocity fluctuation intensity and longitudinal correlation coefficient were made and were employed in the comparison of data and in the theoretical calculation of turbulent flame speed.
Date: May 7, 1956
Creator: Mickelsen, William R. & Ernstein, Norman E.
System: The UNT Digital Library
Purex Waste Storage. Part I - 241-A Waste Storage Facilities (open access)

Purex Waste Storage. Part I - 241-A Waste Storage Facilities

Storage of the fission products separated from the product streams of the Purex process is being accomplished using a smaller volume of accompanying solution than any other process here-to-fore used at HAPO. The operating technique and control mechanisms which are needed to store large quantities of these highly radioactive wastes are not yet fully understood, but considerable insight into the problem has been gained from the experience at Redox during the last 36 months. The basic intentions of the 241-A Storage Facility design is to control the boiling wastes by providing suitable tanks to contain the liquid and a vapor system provided with suitable seals to control the vapors. This document (Part I) will present a somewhat detailed description of the Purex Storage Facility and a review of the activities there before plant start-up. Part II, published under separate cover, contains a description of Waste Farm Technology including a process description and a recommended plan for operation.
Date: March 7, 1956
Creator: O'Neill, G. L. & Swift, W. H.
System: The UNT Digital Library