Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude 1: liquid-cooling systems (open access)

Analytical comparison of turbine-blade cooling systems designed for a turbojet engine operating at supersonic speed and high altitude 1: liquid-cooling systems

Report presenting an investigation of the influence of high-altitude supersonic flight on the operation and effectiveness of turbine-blade liquid-cooling systems for application in turbojet engines in guided missiles and in supersonic aircraft. The problems encountered in liquid-cooling systems were investigated with reference to several specific designs for alternate heat-rejection mediums.
Date: February 20, 1953
Creator: Schramm, Wilson B.; Nachtigall, Alfred J. & Arne, Vernon L.
Object Type: Report
System: The UNT Digital Library
Tests in the Ames 40- by 80-Foot Wind Tunnel of an Airplane Model With an Aspect Ratio 4 Triangular Wing and an All-Movable Horizontal Tail - High-Lift Devices and Lateral Controls (open access)

Tests in the Ames 40- by 80-Foot Wind Tunnel of an Airplane Model With an Aspect Ratio 4 Triangular Wing and an All-Movable Horizontal Tail - High-Lift Devices and Lateral Controls

Memorandum presenting tests of a triangular-wing-airplane model equipped with high-lift devices and lateral and directional controls. The model consisted of an aspect ratio 4 triangular wing in combination with a fuselage of fineness ratio 12.5, a thin, triangular, vertical tail with a constant-chord rudder, and a thin, unswept, all-movable horizontal tail. Results regarding the effects of flap deflection and tail incidence on the pitching moment characteristics, lift and drag characteristics, and rudder effects are provided.
Date: February 20, 1953
Creator: Franks, Ralph W.
Object Type: Report
System: The UNT Digital Library
Flight Determination of the Static Longitudinal Stability Boundaries of the Bell X-5 Research Airplane with 59 Degrees Sweepback (open access)

Flight Determination of the Static Longitudinal Stability Boundaries of the Bell X-5 Research Airplane with 59 Degrees Sweepback

"During the flight program on the Bell X-5 airplane with 59 degrees sweepback to determine the practical Mach number and normal-force coefficient limits of this configuration, a reduction in static longitudinal stability was encountered in maneuvering flight. A determination of the boundary for reduction of longitudinal stability extending to a Mach number of 0.98 is presented in this paper. A reduction of static longitudinal stability existed for all elevator and all stabilizer-executed maneuvers" (p. 1).
Date: February 20, 1953
Creator: Finch, Thomas W. & Walker, Joseph A.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-9 (open access)

Texas Attorney General Opinion: S-9

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: Necessity that the presiding judge of an administrative district be redesignated when his term as district judge is extended by his re-election.
Date: February 20, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Preliminary Results of the Ratio of PU²³⁹ Fission Cross Section to U²³⁵ Fission Cross Section (open access)

Preliminary Results of the Ratio of PU²³⁹ Fission Cross Section to U²³⁵ Fission Cross Section

This report presents the final results from the investigation of the ratio of Pu-239 fission cross section to U-235 fission cross section. Three sets of plutonium and uranium foils were prepared at KAPL and were investigated to acquire the final results.
Date: February 20, 1953
Creator: Leonard, B. R.
Object Type: Report
System: The UNT Digital Library
The Analysis of TBP Process Streams for Calcium with the Flame Photometer (open access)

The Analysis of TBP Process Streams for Calcium with the Flame Photometer

Summary: A method was found for determining calcium concentrations in TBP process streams in spite of serious interferences bysodium, ferrous, uranyl, sulfate, phosphate, and sulfamate ions as well as by TBP. The precision attainable varied from sample to sample, depending upon its composition. In general, errors of 20% or greater occurred. The smallest determinable amount of calcium was about 10 mg/1.
Date: February 20, 1953
Creator: Brite, D. W.
Object Type: Report
System: The UNT Digital Library
Uranium Oxide Phase Equilibrium Systems (open access)

Uranium Oxide Phase Equilibrium Systems

Abstract: "UO2 and ThO2 form a continuous series of solid solutions with the solidus-liquidus from 2875 C for UO2 to above 3200 C for ThO2."
Date: February 20, 1953
Creator: Lambertson, Wingate A.; Mueller, Melvin H. & Gunzel, Fred H., Jr.
Object Type: Report
System: The UNT Digital Library
Progress Report on the Experimental Breeder Reactor April 1, 1951 Through January 31, 1953 (open access)

Progress Report on the Experimental Breeder Reactor April 1, 1951 Through January 31, 1953

This report describes the progress on the experimental breeder reactor. It focuses on the approach to critical experiments, calibration of controls and flues and flux distributions.
Date: February 20, 1953
Creator: Lichtenberger, H. V.; Novick, M.; Cerutti, B. C.; Cameron, R. A.; McGinnis, D. F.; Pettitt, E. N. et al.
Object Type: Report
System: The UNT Digital Library