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COLLECTION OF AEROSOLS BY FIBER MATS. TECHNICAL REPORT NO. II (open access)

COLLECTION OF AEROSOLS BY FIBER MATS. TECHNICAL REPORT NO. II

None
Date: October 31, 1953
Creator: Wong, J. B. & Johnstone, H. F.
System: The UNT Digital Library
DEVIATIONS FROM THERMAL EQUILIBRIUM IN SHOCK WAVES (open access)

DEVIATIONS FROM THERMAL EQUILIBRIUM IN SHOCK WAVES

None
Date: October 31, 1953
Creator: Bethe, H.A. & Teller, E.
System: The UNT Digital Library
DIVISION OF BIOLOGICAL AND MEDICAL RESEARCH QUARTERLY REPORT FOR MAY, JUNE, JULY, 1952 (open access)

DIVISION OF BIOLOGICAL AND MEDICAL RESEARCH QUARTERLY REPORT FOR MAY, JUNE, JULY, 1952

None
Date: October 31, 1953
Creator: Brues, A.M. ed.
System: The UNT Digital Library
FIRST QUARTERLY REPORT ON RADIATION DAMAGE RESEARCH FOR JULY 1 TO SEPTEMBER 30, 1952 (open access)

FIRST QUARTERLY REPORT ON RADIATION DAMAGE RESEARCH FOR JULY 1 TO SEPTEMBER 30, 1952

None
Date: October 31, 1953
Creator: unknown
System: The UNT Digital Library
The Inventory of Electromagnetically Enriched Isotopes: October 31, 1953 (open access)

The Inventory of Electromagnetically Enriched Isotopes: October 31, 1953

None
Date: October 31, 1953
Creator: Keim, C. P.; Normand, C. E. & Weaver, B.
System: The UNT Digital Library
Methods of Treatment of Displacement Integral Equations (open access)

Methods of Treatment of Displacement Integral Equations

None
Date: October 31, 1953
Creator: Frankel, S. & Nelson, E.
System: The UNT Digital Library
QUARTERLY PROGRESS REPORT FOR JULY, AUGUST, AND SEPTEMBER 1952 (open access)

QUARTERLY PROGRESS REPORT FOR JULY, AUGUST, AND SEPTEMBER 1952

None
Date: October 31, 1953
Creator: unknown
System: The UNT Digital Library
RADIATIONS FROM SELENIUM 75 (open access)

RADIATIONS FROM SELENIUM 75

None
Date: October 31, 1953
Creator: Jensen, E.N.; Laslett, L.J.; Martin, D.S. Jr.; Hughes, F.J. & Pratt, W.W.
System: The UNT Digital Library
[Sugarland Industries Cotton Operations: January-October 1953] (open access)

[Sugarland Industries Cotton Operations: January-October 1953]

Monthly report documenting Sugarland Industries operational income, sales, and expenses related to cotton operations.
Date: October 31, 1953
Creator: Sugarland Industries
System: The Portal to Texas History
[Sugarland Industries Cotton Gin Operations: January-October 1953] (open access)

[Sugarland Industries Cotton Gin Operations: January-October 1953]

Monthly report documenting Sugarland Industries operational income and expenses related to cotton gin operations.
Date: October 31, 1953
Creator: Sugarland Industries
System: The Portal to Texas History
[Sugarland Industries Cottonseed Operations: January-October 1953] (open access)

[Sugarland Industries Cottonseed Operations: January-October 1953]

Monthly report documenting Sugarland Industries operational income, sales, and expenses related to cottonseed operations.
Date: October 31, 1953
Creator: Sugarland Industries
System: The Portal to Texas History
Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01 (open access)

Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01

From Introduction: "This paper presents the results of tests made at a Mach number of 2.01 to determine the effect of body length on the longitudinal characteristics (zero roll angle) for five complete configurations as well as for the bodies alone, the bodies plus wings, and the bodies plus canard surfaces. The experimental results are compared with some simple theoretical estimates."
Date: October 30, 1953
Creator: Spearman, M. Leroy
System: The UNT Digital Library
[Herman Lurie's Weekly Report, October 30, 1953] (open access)

[Herman Lurie's Weekly Report, October 30, 1953]

Weekly report discussing the state of the raw sugar market, including details for prices and market fluctuations related to weights in tons, regions, distribution, years, and figures.
Date: October 30, 1953
Creator: Lurie, Herman
System: The Portal to Texas History
[Imperial Sugar Company Estimated Daily Cash Position: October 30, 1953] (open access)

[Imperial Sugar Company Estimated Daily Cash Position: October 30, 1953]

Daily cash report for Imperial Sugar Company including a list of large withdrawals for the months surrounding the date showing the daily expenses and estimated balance for each entry.
Date: October 30, 1953
Creator: Imperial Sugar Company
System: The Portal to Texas History
Pile Neutron Production Field Curves Calculated Using the UCRL Differential Analyzer (open access)

Pile Neutron Production Field Curves Calculated Using the UCRL Differential Analyzer

A set of 69 pile yield curves for the production of plutonium, americium, and curium isotopes in a neutron flux of 5 x 10<sup>14 cm<sup>-2 sec<sup>-1 is given. The differential analyzer of the University of California Radiation Laboratory was used in obtaining the curves. The curves are given also on log-log plots for comparison.
Date: October 30, 1953
Creator: Barrett, R. J.; Killeen, John, 1925-; Rasmussen, J. O. & Thompson, Stanley Gerald, 1912-1976
System: The UNT Digital Library
Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 (open access)

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60

Report presenting an investigation to determine the effect of several seeker-nose configurations on the static longitudinal stability, canard control characteristics, and lift and drag at Mach number 1.60 of a canard-type ramjet missile with 70 degree delta canard control surfaces and 70 degree delta wings. The tests indicate that, for the most part, the configurations tested exhibited no significant difference in static longitudinal stability or horizontal-canard control effectiveness.
Date: October 30, 1953
Creator: Robins, A. Warner
System: The UNT Digital Library
Proton-Proton Scattering at 9.7 Mev (open access)

Proton-Proton Scattering at 9.7 Mev

None
Date: October 30, 1953
Creator: Cork, B. & Hartsough, W.
System: The UNT Digital Library
RESEARCH ON THE RADIATION STABILITY OF ORGANIC FLUIDS. Progress Report for January 1, 1953 through September 30, 1953. Report No. 6 (open access)

RESEARCH ON THE RADIATION STABILITY OF ORGANIC FLUIDS. Progress Report for January 1, 1953 through September 30, 1953. Report No. 6

Additional knowledge was gained pertaining to effects of irradiation variables, chemical components, etc., on the stability of organics. This basic program was supplemented with an applied program wherein research was undertaken of particular irterest in reactor moderator-coolart and lubricant applications. Irradiations of the capsule type in the absence of air were conducted in the MTR, BNL, and X-10 reactors under a variety of conditions in investigations of effects of temperature, flux, dosage, and organic chemical structure. The MTR gamma facility and the California Research Co/sup 60/ source were also used. With highly aromatic organics, damage measured by viscosity change was found independent of irradiation temperature up to 371 deg C. Coke formation was minor, although it was universal at 426 deg C. Many fused ring and nonfused ring aromatics were stable at 371 deg C. Viscosity changes were slight, and gassing amounted to about 2 to 5 ml gas/ml fluid. Simple molecular distillations showed biphenyl, naphthalene, and 1,3-diphenylbenzene, to be 93 to 97% distillable, of which 72 to 81% was pure starting material. The stabilities of solutions of highly viscous polymers in low viscosity alkylbenzenes were studied in the presence of air with gamma radiation. Styrene-alkene copolymer, polyalkene, and polyester …
Date: October 30, 1953
Creator: unknown
System: The UNT Digital Library
Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26 (open access)

Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26

Report presenting a free-flight investigation of a rocket-powered research model to determine the hinge-moment and normal-force characteristics of a trailing-edge control on a delta wing between Mach numbers of 0.50 and 1.26. The hinge-line location of 40 percent control chord satisfactorily reduced the high hinge moments associated with plain flap-type controls. Results regarding hinge moments and normal force are provided.
Date: October 30, 1953
Creator: Martz, C. William & Goslee, John W.
System: The UNT Digital Library
Wake Surveys in the Slipstream of a Full-Scale Supersonic-Type Three-Blade Propeller at Mach Numbers to 0.96 (open access)

Wake Surveys in the Slipstream of a Full-Scale Supersonic-Type Three-Blade Propeller at Mach Numbers to 0.96

Report presenting an investigation of the thrust loading by wake surveys in the slipstream of a full-scale supersonic-type three-blade propeller (the Curtiss-Wright 109622) that was conducted in the transonic tunnel. Integrated-thrust coefficient values were found to be in good agreement with the force data. Results regarding thrust loading at constant advance ratios, at advance ratios for maximum efficiency, and lift-coefficient distribution are also provided.
Date: October 30, 1953
Creator: Swihart, John M. & Norton, Harry T., Jr.
System: The UNT Digital Library
Drag Measurements on Equivalent Bodies of Revolution of Six Configurations of the Convair MX-1964 (Originally MX-1626) Proposed Supersonic Bomber (open access)

Drag Measurements on Equivalent Bodies of Revolution of Six Configurations of the Convair MX-1964 (Originally MX-1626) Proposed Supersonic Bomber

"Tests on equivalent bodies of revolution of six configurations of the Consolidated Vultee Aircraft Corporation proposed supersonic bomber (Convair MX-1964) have indicated that it is possible to reduce the drag of the configuration by designing it to have a favorable area distribution. The method of NACA RM L53I22c to predict the peak pressure drag of a configuration on the basis of its area distribution gave generally good agreement with the subject models" (p. 1).
Date: October 29, 1953
Creator: Hall, James Rudyard
System: The UNT Digital Library
Effect of Inlet-Air Temperature on Performance of a 16-Inch Ram-Jet Combustor (open access)

Effect of Inlet-Air Temperature on Performance of a 16-Inch Ram-Jet Combustor

Report presenting an investigation of the effect of inlet-air temperature on the combustion efficiency of a 16-inch ram-jet engine in a connected-pipe installation. The engine was operated over a range of fuel-air ratios with several different combustor configurations and two fuel types. Configurations tested included a sloping baffle and a can-type combustor in three configurations.
Date: October 29, 1953
Creator: Cervenka, A. J.; Dangle, E. E. & Friedman, Robert
System: The UNT Digital Library
Effective Thermal Conductivities of Magnesium Oxide Stainless Steel, and Uranium Oxide Powders (open access)

Effective Thermal Conductivities of Magnesium Oxide Stainless Steel, and Uranium Oxide Powders

Memorandum presenting testing conducted to determine the conductivity of magnesium oxide, stainless steel, and uranium oxide powders in various gases at a range of temperatures. Results regarding the experimental effective conductivities, comparison of analytical and experimental results, and effect of pressure on conductivity are provided.
Date: October 29, 1953
Creator: Eian, C. S. & Deissler, R. G.
System: The UNT Digital Library