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Atmospheric Contamination Associated with Inert-Gas-Shielded, Consumable Electrode Welding

Description: Apparent excessive concentrations of atmospheric contamination which were reported to be associated with an inert-gas-shielded consumable electrode arc wielding operation were studied to evaluate the potential health hazards. A study was made of the concentrations of metal fume and gaseous products of the operation as well as the spectrum of ultraviolet radiation. Recommendations for necessary controls were made.
Date: July 25, 1955
Creator: Adley, F. E. & Gill, W. E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Envelope for Advance Pattern #8395

Description: Advance pattern to make a misses' and womens' shirtwaist dress, street length with short sleeves, center front button closure and contour belt including illustrations of the finished pieces and information about sizing and construction on the back.
Date: 1955/1959
Creator: Advance Pattern Co., Inc.
Item Type: Refine your search to only Text
Partner: UNT College of Visual Arts + Design

Evening clutch

Description: Clutch style evening handbag of white and gold brocade with fleur de lis inspired pattern. Rectangular inverted frame. Flip clip closure of gold tone metal with silver mounted rhinestone cluster center. Alternate handle of metallic gold serpentine chain attached at inside of handbag by fasteners of metallic gold. Lined in dark gold satin with one patch pocket. Coin purse of matching dark gold satin with brass ball twist closure and inverted light gold frame matching lining of coin purse; attach… more
Date: 1955/1975
Creator: After Five
Item Type: Refine your search to only Physical Object
Partner: UNT College of Visual Arts + Design

Handbag

Description: Clutch handbag of black satin. Rectangular inverted frame; alternative gold tone chain handle on interior. Flip clip closure of metallic gold with clear cylindrical lucite center. Lining of black satin with one pocket. Attached coin purse of black satin with lining of gold colored fabric; brass ball twist closure. Maker's stamp: After/ Five / Made in / U.S.A. Width: 7 3/4" Height: 5 1/2" Depth: 3/4"
Date: 1955/1965
Creator: After Five
Item Type: Refine your search to only Physical Object
Partner: UNT College of Visual Arts + Design
open access

The Theories of Turbulence

Description: "The theory of turbulence reached its full growth at the end of the 19th century as a result of the work by Boussinesq and Reynolds. It then underwent a long period of stagnation which ended under the impulse given to it by the development of wind tunnels caused by the needs of aviation. Numerous researchers, attempted to put Reynolds' elementary statistical theory into a more precise form. During the war, some isolated scientists - von Weizsacker and Heisenberg in Germany, Kolmogoroff in Russi… more
Date: October 1955
Creator: Agostini, L. & Bass, J.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Analysis of the Horizontal-Tail Loads Measured in Flight on a Multiengine Jet Bomber

Description: "The primary objectives of the present paper are to report the horizontal-tail-loads measurements for configuration B which have not previously been reported and to summarize the horizontal-tail-loads results obtained with both configurations. The manner in which the aerodynamic-loads data were analyzed to include structural temperature effects and fuselage flexibility effects constitutes an important part of the present paper" (p. 1).
Date: September 1955
Creator: Aiken, William S., Jr. & Wiener, Bernard
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Reaction of Hydrogen With Uranium

Description: Report discussing reaction of hydrogen with uranium in a range of temperatures and pressures. Experimental materials, methods and results are included.
Date: February 17, 1955
Creator: Albrecht, William M. & Mallett, Manley William, 1909-
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Effects of Wing-Fuselage Flow Fields on Missile Loads at Subsonic Speeds

Description: "The flow-field characteristics around a swept-wing airplane model at low subsonic speed are described, and the loads induced on a typical missile model while operating within these flow fields are presented. In addition, theoretical flow fields are compared with experiment and are used in first-order estimations of the resulting induced missile loads" (p. 1).
Date: June 27, 1955
Creator: Alford, William J., Jr.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching From the Midsemispan and Wing-Tip Locations of a 45 Degree Sweptback Wing-Fuselage Combination

Description: Report presenting an investigation at low speed to determine the static aerodynamic forces and moments on a canard missile model during launching from the midsemispan and wing-tip locations of a wing-fuselage combination with a 45 degree sweptback wing. When the missile was mounted under the wing at the midsemispan location, changes in chordwise position produced large changes in missile forces and moments.
Date: April 6, 1955
Creator: Alford, William J., Jr.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching From the 25-Percent-Semispan and Wing-Tip Location of a 45 Degree Sweptback Wing-Fuselage Combination

Description: Report presenting an investigation at low speed in the 300 mph tunnel to determine the static aerodynamic forces and moments on a missile model during simulated launching from 25-percent-semispan and wing-tip locations of a wing-fuselage combination. Results regarding the differences in location and effects induced by the fuselage are provided.
Date: May 25, 1955
Creator: Alford, William J., Jr.; Silvers, H. Norman & King, Thomas J., Jr.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department

Hat

Description: Hat in calot style of beige satin; small rhinestones interspersed with seed pearls form a radiating design from center of crown; dangling pearl trims around edge. Label: Alfreda New York. Label: Innes Wichita
Date: 1955
Creator: Alfreda Hats (New York, New York)
Item Type: Refine your search to only Physical Object
Partner: UNT College of Visual Arts + Design
open access

A method for the analysis of compounds containing boron, carbon, and hydrogen

Description: Report presenting a method for analyzing each of the elements, boron, carbon, and hydrogen from the quantitative analysis of a single sample of an organoboron compound. The method is helpful for the analysis of volatile hydrocarbons and polynuclear aromatic compounds.
Date: March 3, 1955
Creator: Allen, Harrison, Jr. & Tannenbaum, Stanley
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Chemical and Physical Properties of Modified Hi-Cal-2

Description: Memorandum presenting some physical and chemical properties of a sample of modified Hi-Cal-2. Some of the results obtained include chemical analysis, heat of combustion, density, freezing point, self-ignition temperature, flash point, oxygen stability, water stability test, infrared spectrum, and vapor pressure and decomposition are provided.
Date: December 1955
Creator: Allen, Harrison, Jr.; McDonald, Glen E. & Pusanski, Barbara J.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Visualization study of secondary flows in turbine rotor tip regions

Description: Report presenting a visualization study using smoke to see the secondary-flow phenomena in the rotor-blade tip region of a low-speed turbine. Measurements of the factors affecting the flow patterns were recorded from visual observations. Results regarding a general description of the smoke patterns, shroud boundary-layer considerations, transition rotor tip speed, and high-speed-turbine operating conditions are provided.
Date: September 1955
Creator: Allen, Hubert W. & Kofskey, Milton G.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Preliminary investigation of effect on performance of dividing conical-spike nose inlets into halves at Mach numbers 1.5 to 2.0

Description: Inserting a splitter plate in the subsonic diffuser caused a pressure-recovery loss of about 1 percent for an inlet with a long nearly constant-area throat section. The loss was due to the increased surface area. Another inlet, which had a comparatively rapid area increase immediately after the throat, experienced pressure-recovery losses of 5 and 6 percent at Mach numbers of 1.8 and 2.0, respectively, and about 1 percent at Mach 1.5.
Date: December 19, 1955
Creator: Allen, John L.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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