Fundamental Flashback, Blowoff, and Yellow-Tip Limits of Fuel Gas-Air Mixtures (open access)

Fundamental Flashback, Blowoff, and Yellow-Tip Limits of Fuel Gas-Air Mixtures

Report issued by the Bureau of Mines over experiments conducted on fuel-gas mixtures. The results of these experiments are presented. This report includes tables, graphs, illustrations, and photographs.
Date: July 1956
Creator: Grumer, Joseph; Harris, Margaret E. & Rowe, Valeria R.
Object Type: Report
System: The UNT Digital Library
The Properties of Uranium Containing Minor Additions of Aluminum or Zirconium (open access)

The Properties of Uranium Containing Minor Additions of Aluminum or Zirconium

This report discusses studies revealing the tensile properties, hot hardness, and heat treatment characteristics of uranium alloys with added aluminum or zirconium.
Date: July 16, 1956
Creator: Saller, Henry A.; Rough, Frank A. & Chubb, Walston
Object Type: Report
System: The UNT Digital Library
Investigation of Ammonium Uranates (open access)

Investigation of Ammonium Uranates

This report studies ammonium dichromate and the conditions it needs to be under in order to precipitate and be isolated from an aqueous system.
Date: July 19, 1956
Creator: Ewing, Robert A.; Kiehl, Samuel J. & Bearse, Arthur E.
Object Type: Report
System: The UNT Digital Library
The Properties and Heat Treatment of Uranium-Titanium Alloys (open access)

The Properties and Heat Treatment of Uranium-Titanium Alloys

This report discusses mechanical properties and heat treatment of some uranium-titanium alloys. These alloys were tested for use as fuel-element material.
Date: July 10, 1956
Creator: Douglass, David L.; Marsh, Lyle L. & Manning, George K.
Object Type: Report
System: The UNT Digital Library
Effect of Ceramic or Metal Additives in High-UOâ‚‚ Bodies (open access)

Effect of Ceramic or Metal Additives in High-UOâ‚‚ Bodies

The following report focuses on research made to determine whether the service performance of UOâ‚‚ fuel-elements cores for the PWR can be improved by certain ceramic or metal additions.
Date: July 24, 1956
Creator: Bowers, Donald J.; Hedden, Walter A.; Snyder, M. Jack & Duckworth, Winston H.
Object Type: Report
System: The UNT Digital Library
Selected Annotated Bibliography of the Uranium Geology of Igneous and Metamorphic Rocks in the United States and Territories (open access)

Selected Annotated Bibliography of the Uranium Geology of Igneous and Metamorphic Rocks in the United States and Territories

From introduction: This bibliography is an annotated list of selected reports that were publicly available as of May 31, 1956, pertaining to the uranium content and/or radioactivity of igneous and metamorphic rocks and minerals in the United States.
Date: July 1956
Creator: Curtis, Diane
Object Type: Report
System: The UNT Digital Library
Alpha-Decay Studies in the Heavy Element Region (open access)

Alpha-Decay Studies in the Heavy Element Region

Thesis describing a research conducted to extend observations on nuclear energy levels and how they effect the nucleus itself, and an investigation on the gamma rays associated for the even-even isotopes and to obtain additional data for the oddmass neclei in the hope that more regularities will become apparent for that class of nuclides.
Date: July 3, 1956
Creator: Hummel, John Philip
Object Type: Thesis or Dissertation
System: The UNT Digital Library
Linear Pinch Work in Berkeley (open access)

Linear Pinch Work in Berkeley

The following report discusses the data of the Z-field pick-up loop, an effective diagnostic tool introduced to help experiments with the linear pinch.
Date: July 1956
Creator: Anderson, O. A. & Baker, W. R.
Object Type: Report
System: The UNT Digital Library
Some Preliminary Investigations in the Use of a Supersonic Mercury Vapor Jet for Providing an Energetic Neutral Beam (open access)

Some Preliminary Investigations in the Use of a Supersonic Mercury Vapor Jet for Providing an Energetic Neutral Beam

Report discussing experiments conducted under the Livermore "Waldo" project to determine "(1) surface densities attainable in a supersonic mercury vapor jet stream, (2) the approximate efficiency of a mercury jet for neutralizing a proton beam, and (3) the mercury partial pressure contribution in the bore due to side streaming from the mercury jet."
Date: July 18, 1956
Creator: Steinhaus, J. F.
Object Type: Report
System: The UNT Digital Library
Preliminary Report on a Uranium Occurrence and Regional Geology in the Cherry Creek Area, Gila County, Arizona (open access)

Preliminary Report on a Uranium Occurrence and Regional Geology in the Cherry Creek Area, Gila County, Arizona

Introduction: A reconnaissance of the Black Brush property was made by geologists of the Atomic Energy Commission in March, 1955. This anomalous area was located by an earlier airborne radiometric survey. the examination consisted of preliminary sampling and surface and underground radiometric traversing.
Date: July 1956
Creator: Sharp, Byron J.
Object Type: Report
System: The UNT Digital Library
Polonium (open access)

Polonium

From foreword: This is a report on the efforts of Monsanto Chemical Co. to solve some of the chemical problems involved in the atomic energy program.
Date: July 1956
Creator: Moyer, Harvey Vernon; Gnagey, Lloyd B. & Rogers, Adrian J.
Object Type: Report
System: The UNT Digital Library
Effect of Wing Size and Amount of Indentation on Applicability of Transonic Area Rule to Swept-Wing Configurations (open access)

Effect of Wing Size and Amount of Indentation on Applicability of Transonic Area Rule to Swept-Wing Configurations

Memorandum presenting a systematic transonic zero-lift drag investigation utilizing a swept-wing configuration with three different ratios of wing to fuselage size utilizing a 6-inch helium gun. The experiments and comparisons with other results indicated that the reduction of pressure drag obtainable from partial indentation is approximately proportional to the amount of indentation employed up to a Mach number of 1.3. Results regarding the basic data, total drag, pressure drag, equivalent bodies, and special projections are provided.
Date: July 20, 1956
Creator: Hall, James Rudyard
Object Type: Report
System: The UNT Digital Library
Force and Pressure-Distribution Investigation to High Angles of Attack on All-Movable Triangular and Rectangular Wings in Combination With a Body at Supersonic Speeds (open access)

Force and Pressure-Distribution Investigation to High Angles of Attack on All-Movable Triangular and Rectangular Wings in Combination With a Body at Supersonic Speeds

Force and pressure distribution studies to high angles of attack on all-movable triangular and rectangular wings in combination with body at supersonic speeds. The ranges of aspect ratios were, for the triangular wings, 3/8 to 4, and for the rectangular wings, 1 to 3.
Date: July 10, 1956
Creator: Hill, William A., Jr. & Kaattari, George E.
Object Type: Report
System: The UNT Digital Library
Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages (open access)

Some Considerations Regarding the Application of the Supersonic Area Rule to the Design of Airplane Fuselages

Memorandum presenting certain considerations and techniques pertinent to the application of the supersonic area rule to the design of airplane fuselages. Some of the factors considered are an extension of the rule to account for the interference effects of the wing and tail on the general flow field for asymmetrical configurations, the determination of fuselage area developments which result in approximately the minimum wave drag, and the influence of wing parameters and design Mach number on the effectiveness of fuselage shaping.
Date: July 3, 1956
Creator: Whitcomb, Richard T.
Object Type: Report
System: The UNT Digital Library
Static Longitudinal and Lateral Stability Characteristics Including Effects of Transonic Area Rule and Wing Modification of a 0.10- Scale Model of the Douglas A4D-1 Airplane at Transonic Speeds (open access)

Static Longitudinal and Lateral Stability Characteristics Including Effects of Transonic Area Rule and Wing Modification of a 0.10- Scale Model of the Douglas A4D-1 Airplane at Transonic Speeds

Report discussing testing of a model of the Douglas A4D-1 to investigate the static longitudinal characteristics of wing and fuselage modifications and the static lateral characteristics of the basic model.
Date: July 6, 1956
Creator: Bollech, Thomas V. & Wornom, Dewey E.
Object Type: Report
System: The UNT Digital Library
Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0 (open access)

Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0

Translating spike inlet air flow regulation characteristics from transonic to supersonic speeds at zero angle of attack.
Date: July 24, 1956
Creator: Nettles, J. C.
Object Type: Report
System: The UNT Digital Library
The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-Engine Tractor Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10 (open access)

The Effects of Compressibility on the Upwash at the Propeller Planes of a Four-Engine Tractor Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10

Report presenting an investigation in which upflow angles were measured along the horizontal center lines of the propeller planes of a semispan model representing a multiengine airplane with tractor propellers. Testing occurred at a range of Mach and Reynolds numbers. Results regarding the theoretical methods and a comparison of experimental and theoretical results are provided.
Date: July 1956
Creator: Lopez, Armando E. & Dickson, Jerald K.
Object Type: Report
System: The UNT Digital Library
Effect of Phosphate Coatings on Temperature of Metal Parts Exposed to Flame Environments (open access)

Effect of Phosphate Coatings on Temperature of Metal Parts Exposed to Flame Environments

Note presenting an investigation of the effect of phosphate coatings on the temperature of metal specimens placed in a flame. Small cylindrical specimens of mild steel and S-816 alloy were placed in a natural-gas-air flame at specific temperatures. Special attention is given to the fact that temperature drop was noted in certain specimens and the potential reasons for this reaction are explored.
Date: July 1956
Creator: Fryburg, George C.; Katz, Norman H. & Simon, Sidney L.
Object Type: Report
System: The UNT Digital Library
Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data (open access)

Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data

Report presenting a description and comparison of several methods of obtaining the time response of linear systems to either a unit impulse or an arbitrary input from frequency-response data. All of the methods give good accuracy when applied to a second-order system; the main difference is the required computing time.
Date: July 1956
Creator: Donegan, James J. & Huss, Carl R.
Object Type: Report
System: The UNT Digital Library
Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8 (open access)

Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8

Note presenting a program to investigate the aerodynamic heat transfer of a non-isothermal hemisphere-cylinder in the 11-inch hypersonic tunnel at a Mach number of 6.8. Results regarding pressure distribution, laminar recovery factor, temperature distribution, heat-transfer parameters, average heat-transfer coefficient, and schileren observations.
Date: July 1956
Creator: Crawford, Davis H. & McCauley, William D.
Object Type: Report
System: The UNT Digital Library
Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90 (open access)

Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90

Report presenting turbulent-heat-transfer measurements obtained through the use of an axially symmetric annual nozzle consisting of an inner shaped center body and an outer cylindrical sleeve at Mach number 3.90. Results regarding the variation of wall temperature with longitudinal distance, variation of local Nusselt number with local Reynolds number, and variation of local temperature-recovery factor with local Reynolds number are provided.
Date: July 1956
Creator: Brevoort, Maurice J.
Object Type: Report
System: The UNT Digital Library
Bending Tests of Ring-Stiffened Circular Cylinders (open access)

Bending Tests of Ring-Stiffened Circular Cylinders

Twenty-five ring-stiffened circular cylinders were loaded to failure in bending. The results are presented in the form of design curves which are applicable to cylinders with heavy rings that fail as a result of local buckling.
Date: July 1956
Creator: Peterson, James P.
Object Type: Report
System: The UNT Digital Library
Three-dimensional transonic flow theory applied to slender wings and bodies (open access)

Three-dimensional transonic flow theory applied to slender wings and bodies

Report presenting the derivation of the integral equations for transonic flow around slender wings and bodies of revolution, with special attention paid to conditions resulting from the presence of shock waves and to the reduction of the relations to the special forms necessary for the discussion of sonic flow.
Date: July 1956
Creator: Heaslet, Max A. & Spreiter, John R.
Object Type: Report
System: The UNT Digital Library
Preliminary investigation of the effects of external wing fuel tanks on ditching behavior of a sweptback-wing airplane (open access)

Preliminary investigation of the effects of external wing fuel tanks on ditching behavior of a sweptback-wing airplane

Report presenting an experimental investigation using a model of a typical sweptback-wing airplane equipped with external wing fuel tanks to determine the effects of the tanks on the ditching behavior. Tanks of various fuel capacity and several shape modifications were used. Results regarding the basic model and original 206-gallon tanks, 450-gallon tanks, 260-gallon tanks, and general effects observed are provided.
Date: July 1956
Creator: McBride, Ellis E.
Object Type: Report
System: The UNT Digital Library