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Alloys of Uranium with Zirconium, Chromium, Columbium, Vanadium, and Molybdenum
Abstract: Information on five uranium binary alloy systems has been surveyed. These systems are the alloys of uranium with zirconium, chromium, columbium, vanadium, and molybdenum. The equilibrium diagrams are discussed, and where available, data have been included on diffusion studies, cladding experiments, and mechanical properties.
Date:
June 19, 1952
Creator:
Saller, Henry A. & Rough, Frank A.
System:
The UNT Digital Library
Alloys of Uranium With Zirconium, Chromium, Columbium Vanadium, and Molybdenum
None
Date:
June 19, 1952
Creator:
Saller, H. A. & Rough, F. A.
System:
The UNT Digital Library
An analysis of axial- and centrifugal-flow turbojet-engine performance with variable-area exhaust nozzle
From Introduction: "The purpose of this report is to compare the effect on engine performance of the variable-area exhaust nozzle for axial- and centrifugal-flow turbojet engines."
Date:
June 19, 1952
Creator:
Barson, Zelmar
System:
The UNT Digital Library
Supplementary Bibliography of NACA Reports Related to Instrumentation and Research Techniques
Memorandum listing NACA reports related to a variety of research topics, including instruments, research equipment, and research techniques.
Date:
June 19, 1952
Creator:
The Division of Research Information
System:
The UNT Digital Library
Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed 2: velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area
Report presenting an investigation of whether or not a two-stage turbine with the frontal area no larger than the compressor frontal area could be satisfactorily designed to drive a particular compressor under take-off conditions. The low blade-tip speed, high work, and high air flow per unit of frontal area of the compressor make it critical that a two-stage turbine is designed to drive it. Results regarding the effect of work division, effect of variation in cone angle, and effects of radial variations on velocity diagrams are provided.
Date:
June 19, 1952
Creator:
Davison, Elmer H. & English, Robert E.
System:
The UNT Digital Library
Drag of circular cylinders for a wide range of Reynolds numbers and Mach numbers
From Summary: "Pressure distributions around circular cylinders placed perpendicular to the stream for subsonic and supersonic flow conditions have been obtained. Drag coefficients calculated from these wind-tunnel tests and from transonic free-flight tests are presented. Drag data are presented for the Mach number range of 0.3 to 2.9."
Date:
June 19, 1952
Creator:
Gowen, Forrest E. & Perkins, Edward W.
System:
The UNT Digital Library
Reaction of Graphic with Sodium
Most of the publications in the open literature available to us agree that sodium does not readily react with graphite, though potassium, rubidium, and cesium readily enter between the planes of the graphite lattice. In view of the conflicting evidence available, it seems inadvisable without very extensive further study to consider the use of graphite in direct contact with liquid sodium, except under very mild conditions of temperature and irradiation, and then only with very pure sodium and completely graphitized graphite.
Date:
June 19, 1952
Creator:
Montet, G. L.
System:
The UNT Digital Library