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NACA Research Memorandums
181
Atomic Energy Commission Reports
66
Hanford Works Reports
32
HW (Series)
27
NACA Technical Reports
25
University of California Radiation Laboratory Reports
24
Oak Ridge National Laboratory Reports
19
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16
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Natural Steam and Geothermal Power Generation : [bibliography]
The following document is a bibliography containing a collection of documents discussing natural steam and geothermal power generation.
Date:
July 25, 1958
Creator:
Maynard, G. R.
Object Type:
Report
System:
The UNT Digital Library
Evaluation of The Texas Company Airborne Radioactivity Survey at Blanding, Utah
Purpose and scope: The purpose of this report is to present an analysis and evaluation of the airborne radioactivity survey of the Blanding, Utah district conducted by The Texas Company on behalf of the Atomic energy Commission. Within the scope of the report, only the results of the airborne survey and the data used in its evaluation are presented. No attempt is made to discuss the details of the survey or of the drilling program conducted in the area. A separate report by P. 1. Melanoon, on the drilling program is in preparation.
Date:
April 25, 1952
Creator:
Rosenzweig, Abraham
Object Type:
Report
System:
The UNT Digital Library
Liquid Metal Fuel Reactor Experiment Annual Technical Report: 1958
Annual report of the Liquid Metal Fuel Reactor Experiment describing progress during calendar year 1958 and as well as an evaluation of progress and plans for future work.
Date:
March 25, 1959
Creator:
Babcock & Wilcox Company
Object Type:
Report
System:
The UNT Digital Library
Effects of Elevated Temperatures on the Properties of Portland Cement Mixtures Related to Surface Removal and Decontamination
From abstract: The effect of heat on the surface removal of concrete was studied by conducting brush tests on samples which had been subjected to prolonged high temperatures in an oven or in direct contact with an oxy-propane flame. Other methods of heat-treating surface layers of concrete were investigated by direct application of an oxy-aluminum torch on the surface and by the exothermic chemical reactions of pyrotechnic compositions placed directly on the surface.
Date:
August 25, 1955
Creator:
Heiskell, R. H.; Black, R. H.; Crew, R. J. & Lee, H.
Object Type:
Report
System:
The UNT Digital Library
Injection and Trapping of High Current Electron Beams
The following report describes the injection and trapping of high current electron beams in order to construct an electron gun and the first 2 Mev section of the accelerator.
Date:
January 25, 1960
Creator:
Christofilos, Nicholas C.
Object Type:
Report
System:
The UNT Digital Library
The Properties and Irradiation Behavior of U₃Si₂
Abstract: A limited study of the compound U₃Si₂ has been made in reference to its use as a prospective nuclear fuel in sodium cooled reactors.
Date:
July 25, 1965
Creator:
Shimizu, H.
Object Type:
Report
System:
The UNT Digital Library
Calculations of the Madelung Constant and Inverse Twelfth Power Repulsion Factors for the Wurtzite Crystal Structure
From abstract: The Madelung constant and the inverse twelfth power repulsion factor have been calculated for the wurtzite structure for wide ranges of the crystal parameters and u.
Date:
July 25, 1965
Creator:
Gehman, William G.
Object Type:
Report
System:
The UNT Digital Library
Large SGR Control Rod Development
From abstract: A development program was initiated to design, fabricate and test an absorber column with a 10 to 12 year lifetime, for use in the proposed LSGR.
Date:
July 25, 1965
Creator:
Dermer, M. D.
Object Type:
Report
System:
The UNT Digital Library
Eta Temperature Effect
The temperature coefficient of eta has been measured with the thermal column of the Argonne pile using uranium foils of different isotopic ratios. The temperature change was effected by filtering neutrons through silver. The measured fractional change per degree centigrade is [formula].
Date:
February 25, 1944
Creator:
Bragdon, E. W.; Hughes, D. & Marshall, John
Object Type:
Report
System:
The UNT Digital Library
A Final Report on the Experiment : the Penetration of Graphite of Different Purities by Lead Bismuth Eutectic
Bi-Pb eutectic and pure Bi penetration of graphites of various densities under 300 degrees C and pressures up to 20 psi was found be of the order of magnitude of 1.0 g/cm(2) and was uniform throughout the graphite. Bi was absorbed less than the eutectic but the oxidation rate of Bi would be prohibitive. There was heavy nitriding in N atmospheres with the Bi and the eutectic.
Date:
September 25, 1944
Creator:
Stroud, William G.
Object Type:
Report
System:
The UNT Digital Library
Preliminary Report on the Hydrolytic Behavior of Cerium (IV)
The following report analyzes the hydrolytic behavior of cerium and compares them with the actinides of uranium and plutonium.
Date:
May 25, 1948
Creator:
Kraus, K. A.; Holmberg, R. W. & Nelson, F.
Object Type:
Report
System:
The UNT Digital Library
Studies of Porphyrin Metabolism, 3. The Relation of Erythropoiesis to the Excretion of Coproporphyrin by Dogs and Rabbits, and to the Concentration of Coproporphyrin and Protoporphyrin in Rabbit Erythrocytes
Report discussing studies regarding porphyrin excretion and hemoglobin metabolism in animals with phenylhydrazine anemia, and studies regarding the coproporphyrin and protoporphyrin in the red blood cells of rabbits.
Date:
November 25, 1945
Creator:
Schwartz, Samuel; Glickman, Marcia; Hunter, Rosie & Wallace, Jean
Object Type:
Report
System:
The UNT Digital Library
The Ratio of Amino Acid Nitrogen to Creatinine in the Urine as a Sensitive Test for Uranium Poisoning
Report discussing experiments that were performed to determine whether amino acids in urine could be used as a test of subtle uranium poisoning.
Date:
May 25, 1948
Creator:
Berke, Harry & Rothstein, A.
Object Type:
Report
System:
The UNT Digital Library
Gas-Cooled Marine Nuclear Power Plant: Interim Report. Project 16
From preface: The principal portion of this report is the scientific and engineering description of a novel reactor and power-plant scheme which was proposed by General Atomic in response to an invitation of the Maritime Administration.
Date:
January 25, 1957
Creator:
Thompson, W. I.; Adler, F.; Case, K.; Bond, W. H.; Creutz, E. C.; Hale, E. A. et al.
Object Type:
Report
System:
The UNT Digital Library
Prestressed Concrete Reactor Vessel Model 1
From introduction: The goal of engineers associated with nuclear power plants is the achievement of safe plants with low generating costs.One possible means of lowering costs is to increase the power generating capability for a single generating unit. To accomplish this, the sizes of nuclear reactors have been increased.
Date:
October 25, 1966
Creator:
unknown
Object Type:
Report
System:
The UNT Digital Library
Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph
Report presenting testing of a towed airplane model in the 19-foot pressure tunnel in conjunction with the development of a flutter testing technique. The model was equipped with an autopilot to keep the model flying straight and level in the tunnel while restrained only in drag. Results regarding period and cycles to damp to half amplitude, time histories, and motions of the flexible wing model are provided.
Date:
March 25, 1955
Creator:
Schneider, William C.
Object Type:
Report
System:
The UNT Digital Library
Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
Report presenting lift, drag, and pitching-moment coefficients, lift-drag ratios, and center-of-pressure positions for four airplane-like configurations determined from tests at a range of Mach numbers and angles of attack. The wings and nose shapes were modified for each of the configurations.
Date:
April 25, 1955
Creator:
Neice, Stanford E.; Wong, Thomas J. & Hermach, Charles A.
Object Type:
Report
System:
The UNT Digital Library
Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed
Report presenting flight measurements of the pressures on the horizontal tail surfaces of a typical propeller-driven pursuit airplane during stalled pull-outs at high Mach number. Unit loads measured on the stabilizer at safe maneuvering limits were not only considerably in excess of the design unit loads, but also occurred in a direction opposite to the design loads. Revision of the tail-load design requirements and manner of specifying safe maneuverability limits to pilots appears necessary.
Date:
April 25, 1944
Creator:
Clousing, Lawrence A. & Turner, William N.
Object Type:
Report
System:
The UNT Digital Library
Effect of inlet-air-flow-distortions on steady-state performance of J65-B-3 turbojet engine
The effects of inlet-air-flow distortions on the performance of the J65-B-3 turbojet engine were determined over a range of altitudes from 15,000 to 50,000 feet at a flight Mach number of 0.8. Radial inlet-air-flow distortions apparently do not affect the radial distribution of pressure after the first few compressor stages, while the circumferential inlet-air-flow distortion carried completely through the engine. For the distortions investigated, at rated exhaust-gas temperature and fixed-area exhaust-nozzle operation, the primary effect of the radial inlet-air-flow distortions was to reduce the engine air flow, and the primary effect of the circumferential distortion was to impose a temperature profile on the turbine, both resulting in reduction of thrust.
Date:
January 25, 1956
Creator:
Smith, Ivan D.; Braithwaite, W. M. & Calvert, Howard F.
Object Type:
Report
System:
The UNT Digital Library
Experimental investigation of effect of cooling air on turbine performance of two turbojet engines modified for air-cooling
Report presenting an investigation at sea-level static conditions to determine the effects of radial discharge of cooling air from turbine rotor blades on turbine performance in two turbojet engines, one with a centrifugal compressor and the other with an axial-flow compressor. Results regarding the performance characteristics, efficiency comparisons, and some interpretation are provided.
Date:
January 25, 1956
Creator:
Smith, Gordon T.; Freche, John C. & Cochran, Reeves P.
Object Type:
Report
System:
The UNT Digital Library
Investigation of the effects of body indentation and of wing-plan-form modification on the longitudinal characteristics of a 60 degree swept-wing-body combination at Mach numbers of 1.41, 1.61, and 2.10
Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel to determine the effects of body indentation on the minimum drag and maximum lift-drag ratio of a 60 degree swept-wing-body combination. A secondary goal of the tests was to determine the effect on the maximum lift-drag ratio of modifying the inboard plan form of the 60 degree swept wing. Lift, drag, and pitching-moment data are presented.
Date:
July 25, 1955
Creator:
Sevier, John R., Jr.
Object Type:
Report
System:
The UNT Digital Library
A flight investigation at transonic speeds and small angles of attack of the aerodynamic characteristics of a model having a 45 degree sweptback wing of aspect ratio 3 with an Naca 64A006 airfoil section
Report presenting an investigation of the longitudinal aerodynamic characteristics of a model with a 45 degree sweptback wing of aspect ratio 3 and a 45 degree sweptback cruciform tail at transonic speeds and small angles of attack by a free-fall recoverable-model technique. Results regarding lift, drag, static longitudinal stability, dynamic longitudinal stability, and loading distribution over the fuselage are provided.
Date:
January 25, 1954
Creator:
Holdaway, George H.
Object Type:
Report
System:
The UNT Digital Library
Investigation of Two Short Annular Diffuser Configurations Utilizing Section and Injection as a Means of Boundary-Layer Control
Memorandum presenting an investigation of the performances of two annular diffuser designs applicable to turbojet afterburner installations to determine the effectiveness of injection and suction boundary-layer controls. Results regarding inlet measurements, flow observations, static-pressure distributions, downstream velocity distributions, and mean performance coefficients are provided.
Date:
January 25, 1955
Creator:
Wilbur, Langley W. & Higginbotham, James T.
Object Type:
Report
System:
The UNT Digital Library
Equilibrium Operating Performance of Axial-Flow Turbojet Engines by Means of Idealized Analysis
"A method of predicting equilibrium operating performance of turbojet engines has been developed, with the assumption of simple model processes for the components. Results of the analysis are plotted in terms of dimensionless parameters comprising critical engine dimensions and over-all operating variables. This investigation was made of an engine in which the ratio of axial inlet-air velocity to compressor-tip velocity is constant, which approximates turbojet engines with axial-flow compressors" (p. 673).
Date:
February 25, 1949
Creator:
Sanders, John C. & Chapin, Edward C.
Object Type:
Report
System:
The UNT Digital Library