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[Estimated Receipts and Melt, December 31, 1953] (open access)

[Estimated Receipts and Melt, December 31, 1953]

Estimated receipts and melt report.
Date: December 31, 1953
Creator: Imperial Sugar Company
System: The Portal to Texas History
[Herman Lurie's Weekly Report, December 31, 1953] (open access)

[Herman Lurie's Weekly Report, December 31, 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: December 31, 1953
Creator: Lurie, Herman
System: The Portal to Texas History
[Herman Lurie's Weekly Report, July 31, 1953] (open access)

[Herman Lurie's Weekly Report, July 31, 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: July 31, 1953
Creator: Lurie, Herman
System: The Portal to Texas History
RADIATION DAMAGE RESEARCH SECOND QUARTERLY REPORT, OCTOBER 1 TO DECEMBER 31, 1952. Quarterly Report 2 (open access)

RADIATION DAMAGE RESEARCH SECOND QUARTERLY REPORT, OCTOBER 1 TO DECEMBER 31, 1952. Quarterly Report 2

None
Date: March 31, 1953
Creator: unknown
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
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
METALLURGY DIVISION QUARTERLY REPORT FOR OCTOBER, NOVEMBER, AND DECEMBER 1953 (open access)

METALLURGY DIVISION QUARTERLY REPORT FOR OCTOBER, NOVEMBER, AND DECEMBER 1953

None
Date: December 31, 1953
Creator: unknown
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
PREPARATION OF CARRIER-FREE LANTHANUM-140 (open access)

PREPARATION OF CARRIER-FREE LANTHANUM-140

None
Date: July 31, 1953
Creator: Salutsky, M.L. & Kirby, H.W.
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
[Imperial Sugar Company, Past Due Accounts, July 31, 1953] (open access)

[Imperial Sugar Company, Past Due Accounts, July 31, 1953]

Past due accounts for Imperial Sugar Company.
Date: July 31, 1953
Creator: Imperial Sugar Company
System: The Portal to Texas History
[Imperial Sugar Company Estimated Daily Cash Position: July 31, 1953] (open access)

[Imperial Sugar Company Estimated Daily Cash Position: July 31, 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. It also lists scheduled payments for bank loans.
Date: July 31, 1953
Creator: Imperial Sugar Company
System: The Portal to Texas History
An Investigation at Transonic Speeds of the Effects of Fences, Drooped Nose, and Vortex Generators on the Aerodynamic Characteristics of a Wing-Fuselage Combination Having a 6-Percent-Thick, 45 Degree Sweptback Wing (open access)

An Investigation at Transonic Speeds of the Effects of Fences, Drooped Nose, and Vortex Generators on the Aerodynamic Characteristics of a Wing-Fuselage Combination Having a 6-Percent-Thick, 45 Degree Sweptback Wing

Report presenting an investigation at transonic speeds to determine the effects of fences, drooped nose, combination fences and drooped nose, and vortex generators on a 45 degree sweptback wing-fuselage combination. The purpose of undertaking this investigation was due to the pitch-up tendency that results from leading-edge vortex-type flow on thin sweptback wings. The data for each component and their interaction with one another is also provided.
Date: March 31, 1953
Creator: Hieser, Gerald
System: The UNT Digital Library
Effect of inlet oxygen concentration on combustion efficiency of J33 single combustor operating with gaseous propane (open access)

Effect of inlet oxygen concentration on combustion efficiency of J33 single combustor operating with gaseous propane

Report presenting an investigation to determine the effect of oxygen concentration of the inlet oxygen-nitrogen mixture on the combustion efficiency of a J33 single combustor operating with gaseous propane fuel. Combustion efficiency data were obtained at a variety of combustion-inlet total pressures, fuel flow rates, and inlet oxygen concentrations. Results regarding combustor data, application of fundamental combustion properties to combustor data, application of simplified reaction kinetics equation to combustor data, comparison of liquid and gaseous fuel data, and limitations of correlation parameters.
Date: March 31, 1953
Creator: Graves, Charles C.
System: The UNT Digital Library
Investigation of the NACA 1.167-(0)(03)-058 and NACA 1.167-(0)(05)-058 Three-Blade Propellers at Forward Mach Numbers to 0.92 Including Effects of Thrust-Axis Inclination (open access)

Investigation of the NACA 1.167-(0)(03)-058 and NACA 1.167-(0)(05)-058 Three-Blade Propellers at Forward Mach Numbers to 0.92 Including Effects of Thrust-Axis Inclination

Report presenting an investigation to determine the aerodynamic characteristics of two three-blade propellers over a range of blade angles and Mach numbers. The thick-blade propeller was more adversely affected by compressibility than the thin-blade propeller, and the maximum efficiency of the thin-blade propeller was higher than the thick-blade propeller.
Date: August 31, 1953
Creator: Demele, Fred A. & Otey, William R.
System: The UNT Digital Library
The effects of fences on the high-speed longitudinal stability of a swept-wing airplane (open access)

The effects of fences on the high-speed longitudinal stability of a swept-wing airplane

Report presenting a series of fence installations tested on a swept-wing jet airplane to determine their effects on the longitudinal instability, or "pitch-up", encountered in high-maneuvering flight. Longitudinal-stability measurements were made at a variety of Mach numbers with nine fence configurations that varied in chordwise extent and spanwise position. Results regarding longitudinal stability, flow phenomena, buffeting and wing dropping, drag, and low-speed stalls are provided.
Date: August 31, 1953
Creator: Bray, Richard S.
System: The UNT Digital Library
A note on secondary flow in rotating radial channels (open access)

A note on secondary flow in rotating radial channels

"A general vector differential equation for the vorticity component parallel to a streamline is derived for steady, nonviscous, and incompressible flow in a rotating system. This equation is then simplified by restricting it to rotating radial channels and by making further simplifying assumptions. The simplified equation is used to solve for the secondary vorticity, the vorticity component parallel to the streamline, in three special cases involving different streamtube geometries; the results are presented in a series of figures" (p. 1).
Date: August 31, 1953
Creator: Kramer, James J. & Stanitz, John D.
System: The UNT Digital Library
Correlation by the Hypersonic Similarity Rule of the Pressure Distributions and Wave Drags for Minimum-Drag Nose Shapes at Zero Angle of Attack (open access)

Correlation by the Hypersonic Similarity Rule of the Pressure Distributions and Wave Drags for Minimum-Drag Nose Shapes at Zero Angle of Attack

Memorandum presenting the use of the hypersonic similarity rule to correlate pressure distributions and wave drags for minimum-drag nose shapes derived by Von Karman and Newton. The computed results have been confirmed by comparison with available experimental data. Wave-drag results for both the Karman and Newtonian shapes are compared with each other and with results for ocnes and circular-arc tangent ogives.
Date: August 31, 1953
Creator: Jorgensen, Leland H.
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
Progress Report No. 30 for May 31, 1953 to August 31, 1953 (open access)

Progress Report No. 30 for May 31, 1953 to August 31, 1953

None
Date: August 31, 1953
Creator: unknown
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
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
Direct Air Blast Exposure Effects in Animals, Operation Upshot-Knothole, Project 4.2 (open access)

Direct Air Blast Exposure Effects in Animals, Operation Upshot-Knothole, Project 4.2

Project 4.2 was designed to study direct (primary) air blast injury, in animals, from an atomic weapon in the range of 20 to 50 psi under circumstances affording protection against missiles, thermal and ionizing radiation and to estimate the probable direct air blast hazard in man. The pressure levels at which atomic weapons direct air blast injuries occur will determine, to a large extent, the number of blast casualties likely to be encountered. It is probable that fatal overpressures are not reached until well within the range at which indirect (secondary) blast, thermal and ionizing radiation are practically certain to prove fatal. Only in special situations affording partial protection from other injuries are blast injuries likely to be of practical importance. Two animal species of widely different body weights (700 rats and 56 dogs) were exposed, together with air pressure recorders, in aluminum cylinders, covered by sandbags and dirt but open at both ends, at seven stations distributed within the intended overpressure range of 20 to 50 psi of Shot 10« About 200 rats were likewise exposed in Shot 9. Unfortunately, the destructive effect of the air blast of Shot 10 was much greater than anticipated. Many of the exposure …
Date: December 31, 1953
Creator: Draeger, R. H. & Lee, R. H.
System: The UNT Digital Library