In-Line Scintillation Gamma Monitor : Preliminary Specifications (open access)

In-Line Scintillation Gamma Monitor : Preliminary Specifications

From introduction: "The following recommendations represent the best estimate, based on present knowledge, of the requirements for generally applicable or "universal" instrument for the continuous monitoring of radioactive process streams in terms of their gamma activity."
Date: January 22, 1953
Creator: Upson, U. L. & Connally, R. E.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: MS-40 (open access)

Texas Attorney General Opinion: MS-40

Letter opinion 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: Validity of House Simple Resolution No. 289, authorizing the expenditure of the contingent funds to purchase a framed copy of the panel picture of the House membership for each member.
Date: May 22, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-71 (open access)

Texas Attorney General Opinion: MS-71

Letter opinion 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; Authority of the Board of Trustees of the Teacher Retirement System to increase membership annuity payments for previously retired teachers in accordance with Section 5 of Senate Bill 334, Acts of 53rd Legislature, 1953.
Date: July 22, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-93 (open access)

Texas Attorney General Opinion: MS-93

Letter opinion 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; Assessment of personal property of an unincorporated bank under the terms of Article 7165, V.C.S.
Date: September 22, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-112 (open access)

Texas Attorney General Opinion: MS-112

Letter opinion 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; Whether Trust Fund Commission for Clayton Vocational Institute is legally in existence.
Date: December 22, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-32 (open access)

Texas Attorney General Opinion: S-32

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: Applicability of the non-communist oath required by H.B. 21, 53rd Legislature, to services by doctors, lawyers, engineers, architects, skilled services, labor, statutory witness fees in criminal cases, payment of expert witnesses, payment for assistance in law enforcement, cooperative projects administered by other agencies, constitutional salaries of State Officers and per diem of members of the Legislature.
Date: April 22, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Hanford Atomic Products Operation monthly report, March 1953 (open access)

Hanford Atomic Products Operation monthly report, March 1953

This is a progress report of the production reactors on the Hanford Reservation for the month of March 1953. This report takes each division (e.g., manufacturing, medical, accounting, occupational safety, security, reactor operations, etc.) of the site and summarizes its accomplishments and employee relations for that month.
Date: April 22, 1953
Creator: McCune, F. K.
Object Type: Report
System: The UNT Digital Library
Hanford Atomic Products Operation monthly report, June 1953 (open access)

Hanford Atomic Products Operation monthly report, June 1953

This document presents a summary of work and progress at the Hanford Engineer Works for June 1953. The report is divided into sections by department. A plant wide general summary is included at the beginning of the report, after which the departmental summaries begin. The Manufacturing Department reports plant statistics, and summaries for the Metal Preparation, Reactor and Separation sections. The Engineering Department`s section summaries work the Technical, Design, and Project Sections. Costs for the various departments are presented in the Financial Department`s summary. The Medical, Radiological Sciences, Utilities and General Services, Employee and Public Relations, and Community Real Estate and Services departments have sections presenting their monthly statistics, work, progress, and summaries.
Date: July 22, 1953
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Calculation of Stagewise Contacting Systems (open access)

Calculation of Stagewise Contacting Systems

From abstract: General expressions relating product stream compositions to the operating conditions of countercurrent stagewise extraction columns are derived by an inductive method, and the conversion of the general equations to ones involving the particular case of constant extraction factor is demonstrated. For comparison, the derivation of simple column equations by the use of finite difference equations is included.
Date: May 22, 1953
Creator: Bloom, J. L. & Auer, P. L.
Object Type: Report
System: The UNT Digital Library
Neon 18 (open access)

Neon 18

None
Date: October 22, 1953
Creator: Gow, J. D. & Alvarez, L. W.
Object Type: Report
System: The UNT Digital Library
Development of Hydrogen-Oxygen Recombiners. Progress Report (open access)

Development of Hydrogen-Oxygen Recombiners. Progress Report

It is the purpose of this report to review our experience with recombiners under actual reactor operating conditions, and to discuss new developments in the field.
Date: October 22, 1953
Creator: Ransohoff, J.A. & Spiewak, I.
Object Type: Report
System: The UNT Digital Library
The Effect of Thyroid Extract on Serum Lipoproteins and Serum Cholesterol (open access)

The Effect of Thyroid Extract on Serum Lipoproteins and Serum Cholesterol

None
Date: October 22, 1953
Creator: Strisower, B.; Gofman, J. W.; Galioni, E. F.; Almada, A. A. & Simon, A.
Object Type: Report
System: The UNT Digital Library
Comparison of Several Methods of Cyclic De-Icing of a Gas-Heated Airfoil (open access)

Comparison of Several Methods of Cyclic De-Icing of a Gas-Heated Airfoil

"Several methods of cyclic de-icing of a gas-heated airfoil were investigated to determine ice-removal characteristics and heating requirements. The cyclic de-icing system with a spanwise ice-free parting strip in the stagnation region and a constant-temperature gas-supply duct gave the quickest and most reliable ice removal. Heating requirements for the several methods of cyclic de-icing are compared, and the savings over continuous ice prevention are shown. Data are presented to show the relation of surface temperature, rate of surface heating, and heating time to the removal of ice" (p. 1).
Date: June 22, 1953
Creator: Gray, Vernon H. & Bowden, Dean T.
Object Type: Report
System: The UNT Digital Library
Examination of Recent Lateral-Stability-Derivative Data (open access)

Examination of Recent Lateral-Stability-Derivative Data

"In the present paper attention is directed to the aerodynamic parameters, the so-called stability derivatives, that affect the lateral behavior of airplanes and missiles. The discussion is centered on three important quantities, the effective-dihedral derivative, the directional-stability derivative, and the damping-in-roll derivative. These quantities are considered for a large angle-of-attack range at subsonic speeds" (p. 1).
Date: October 22, 1953
Creator: Malvestuto, Frank S., Jr. & Kuhn, Richard E.
Object Type: Report
System: The UNT Digital Library
Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds (open access)

Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds

Report presenting longitudinal-damping data in the form of the pitching-moment derivatives and summarized from flight tests of rocket-propelled models and full-scale airplanes. 22 models and 4 airplanes are examined in the study and the damping derivative results are generalized.
Date: January 22, 1953
Creator: Gillis, Clarence L. & Chapman, Rowe, Jr.
Object Type: Report
System: The UNT Digital Library
Hinge-moment characteristics for several tip controls on a 60 degree sweptback delta wing at Mach number 1.61 (open access)

Hinge-moment characteristics for several tip controls on a 60 degree sweptback delta wing at Mach number 1.61

Report presenting an investigation at Mach number 1.61 to determine the hinge-moment characteristics of seven tip controls on a 60 degree sweptback delta wing. Testing occurred over a range of angles of attack and control deflection. The results indicated that the most important parameter in designing delta-wing tip control is the ratio of control-surface area ahead of the hinge line to total control-surface area.
Date: January 22, 1953
Creator: Czarnecki, K. R. & Lord, Douglas R.
Object Type: Report
System: The UNT Digital Library
Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight (open access)

Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight

"During the flight investigation of the X-1 airplane the hinge moments of the elevator and aileron control surfaces have been measured over a Mach number range extending to above 1.0. The results of these measurements are presented in this paper" (p. 2).
Date: June 22, 1953
Creator: Drake, Hubert M. & McKay, John B.
Object Type: Report
System: The UNT Digital Library
Effect of fuels on combustion efficiency of 5-inch ram-jet-type combustor (open access)

Effect of fuels on combustion efficiency of 5-inch ram-jet-type combustor

Report presenting combustion-efficiency data for a 5-inch ramjet-type combustor using a simple V-gutter flame holder. Data for homogeneous fuel-air mixtures of 14 pure fuels and 3 fuel blends cover a range of inlet static pressures and velocities.
Date: May 22, 1953
Creator: Reynolds, Thaine W.
Object Type: Report
System: The UNT Digital Library
An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver (open access)

An analysis of the tracking performances of two straight-wing and two swept-wing fighter airplanes with fixed sights in a standardized test maneuver

From Introduction: "This report presents the initial study, the tracking performance of typical fighter airplanes with fixed gunsights. The types of airplanes tested afford two comparisons of particular interest: that between typical World War II and currently operational fighters of greatly increased speed and altitude, and that between conventional and irreversabile power-boosted controls with artificial feel, both installed on the same airframe."
Date: October 22, 1953
Creator: Rathert, George A., Jr.; Gadeberg, Burnett L. & Ziff, Howard L.
Object Type: Report
System: The UNT Digital Library
Preliminary investigation of the effects of body contouring as specified by the transonic area rule on the aerodynamic characteristics of a delta wing-body combination at Mach numbers of 1.41 and 2.01 (open access)

Preliminary investigation of the effects of body contouring as specified by the transonic area rule on the aerodynamic characteristics of a delta wing-body combination at Mach numbers of 1.41 and 2.01

Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel to determine the effects of body contouring as specified by the transonic drag-rise area rule on the aerodynamic characteristics of a delta wing-body combination at Mach numbers of 1.41 and 2.01. Body contouring reduced zero-lift drag of a delta wing-body combination from that of a basic wing-body combination without contouring by 18 percent at Mach number 1.41 and 6 percent at Mach number 2.01. Results regarding the characteristics at zero lift and characteristics for the lifting condition are provided.
Date: September 22, 1953
Creator: Carlson, Harry W.
Object Type: Report
System: The UNT Digital Library
A Transonic Wind-Tunnel Investigation of the Effect of Modifications to an Indented Body in Combination With a 45 Degree Sweptback Wing (open access)

A Transonic Wind-Tunnel Investigation of the Effect of Modifications to an Indented Body in Combination With a 45 Degree Sweptback Wing

Memorandum presenting an investigation of modifications to an indented body which was originally designed on the basis of the transonic drag-rise rule to determine the effects on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination. The investigation covered a range of Mach numbers and angles of attack. Results regarding lift, drag for the nonlifting case, drag for the lifting case, maximum lift-to-drag ratios, and pitching moment are provided.
Date: September 22, 1953
Creator: Loving, Donald L.
Object Type: Report
System: The UNT Digital Library
The Synthesis of Butylsilanes by a Large-Scale Reduction with Lithium Aluminum Hydride (open access)

The Synthesis of Butylsilanes by a Large-Scale Reduction with Lithium Aluminum Hydride

"Eighty pounds of butylsilanes required for test purposes was synthesized by reducing butyltrichlorosilane with lithium aluminum hydride in dioxane solution. This was safely and successfully accomplished by operating in steel equipment under an atmosphere of oil-pumped nitrogen to minimize the hazards involved in conducting this operation on a large scale. The apparatus and procedure used to carry out the necessary manipulations are described in this report" (p. 1).
Date: July 22, 1953
Creator: Kaye, Samuel; Tannenbaum, Stanley & Hipsher, Harold F.
Object Type: Report
System: The UNT Digital Library
Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5 (open access)

Flight Determination of Drag of Normal-Shock Nose Inlets With Various Cowling Profiles at Mach Numbers From 0.9 to 1.5

Report discussing free-flight tests of normal-shock nose-inlet models with 1-series, parabolic, and conic cowling profiles in order to investigate the external drag characteristics at an angle of attack of 0 degrees. The testing occurred at a variety of Mach numbers, mass-flow ratios, and Reynolds numbers. Information about the effect of afterbody length, basic data, and effect of cowl shape is provided.
Date: October 22, 1953
Creator: Sears, R. I.; Merlet, C. F. & Putland, L. W.
Object Type: Report
System: The UNT Digital Library
Mechanical design analysis of several noncritical air-cooled turbine disks and a corrugated-insert air-cooled turbine rotor blade (open access)

Mechanical design analysis of several noncritical air-cooled turbine disks and a corrugated-insert air-cooled turbine rotor blade

Report presenting a series of turbine wheel designs made for a turbojet engine with an axial-flow compressor. The designs were made to determine the influence of air-cooling on overall engine design, weight, critical-material content, and complexity and to assist with construction of research model full-scale turbines.
Date: July 22, 1953
Creator: Moseson, Merland L.; Krasner, Morton H. & Ziemer, Robert R.
Object Type: Report
System: The UNT Digital Library