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Plastic Flow During Extrusion of Tubing (open access)

Plastic Flow During Extrusion of Tubing

Abstract: "A study of plastic flow during the extrusion of tubing was made by extruding colored Plasticine billets in a small-scale extrusion press. Decreasing the included angle of the conical die and tapering the ram end of the billet decreased the amount of coextrusion of the backer block into the tubing, lubricating the billet also decreased coextrusion."
Date: July 26, 1955
Creator: Saller, Henry A.; Keeler, John R. & Cuddy, Lee J.
System: The UNT Digital Library
Dissolution of Aluminum-Canned Thorium (open access)

Dissolution of Aluminum-Canned Thorium

The following report studies the dissolution of aluminum-canned thorium, providing results that suggest a dissolution cycle that permits the separation of the canned-slug components.
Date: July 26, 1955
Creator: Beach, John G.; Schickner, William C. & Faust, Charles L.
System: The UNT Digital Library
Note on Table Top Injection : High Energy Injection Inside the Mirrors (open access)

Note on Table Top Injection : High Energy Injection Inside the Mirrors

"High energy injection into Table Top is discussed for the case in which the ion sources are to be located inside the mirrors in the mirror region. Two typical ion source geometries are considered. maximum time intervals available for injection indicated are on the order of 7 to 25 microseconds."
Date: August 26, 1955
Creator: Hiskes, J. R.
System: The UNT Digital Library
Water treatment modifications to present areas (open access)

Water treatment modifications to present areas

It is the purpose of this document to review and up-date the previously presented scope basis for the activated silica installations in light of the existence of the Phase I portion and the present expected water flow requirements of Project CG-558. It is the further purpose to outline the recommended scope bases for the sulfuric acid addition system for pH correction at all areas.
Date: January 26, 1955
Creator: Pearl, W. L.
System: The UNT Digital Library
Hanford Atomic Products Operation monthly report, July 1955 (open access)

Hanford Atomic Products Operation monthly report, July 1955

This document presents a summary of work and progress at the Hanford Engineer Works for July 1955. 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 summarizes work for 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: August 26, 1955
Creator: unknown
System: The UNT Digital Library
Permissible Rate of Temperature Rise of Shells (open access)

Permissible Rate of Temperature Rise of Shells

None
Date: May 26, 1955
Creator: Greenstreet, B. L. & Thompson, A. S.
System: The UNT Digital Library
RESEARCH AND DEVELOPMENT IN THE FIELD OF THORIUM CHEMISTRY AND METALLURGY. Monthly Progress Report for March 15 thru April 15, 1955 (open access)

RESEARCH AND DEVELOPMENT IN THE FIELD OF THORIUM CHEMISTRY AND METALLURGY. Monthly Progress Report for March 15 thru April 15, 1955

A transition program, eliminating most of the wet chemical techniques for the preparation of cell feed and replacing these with a high temperature chlorination process, was begun. Crushing tests on a Fitz mill were initiated and tentative conclusions are that this type of equipment as superior to a combination of jaw and roll crushing. Small scale chlorination experiments indicate the feasibility of pelletizing ThOCO/sub 3/ for feed to a eontinuous hightemperature chlorinator. (D.E.B.)
Date: April 26, 1955
Creator: Wyatt, J.L.
System: The UNT Digital Library
BASIC PRINCIPLES INVOLVED IN THE MACRO-SEPARATION OF ADJACENT RARE EARTHS FROM EACH OTHER BY MEANS OF ION EXCHANGE (open access)

BASIC PRINCIPLES INVOLVED IN THE MACRO-SEPARATION OF ADJACENT RARE EARTHS FROM EACH OTHER BY MEANS OF ION EXCHANGE

None
Date: October 26, 1955
Creator: Powell, J.E. & Spedding, F.H.
System: The UNT Digital Library
Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398 (open access)

Effects of various modifications on the static longitudinal stability and control characteristics of a 0.065-scale model of the Chance Vought Regulus II missile at a Mach number of 2.01: TED No. NACA AD 398

Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel to determine the effects on the static longitudinal stability and control characteristics of various modifications to a 0.065-scale model of the Chance Vought Regulus II missile. Some of the modifications included control housing on top of the fuselage, two sizes of canard surfaces with fixed incidence angles, various angles of nose droop, and two types of inlet boundary-layer bleed diverters.
Date: September 26, 1955
Creator: Robinson, Ross B. & Driver, Cornelius
System: The UNT Digital Library
Flight determination of minimum drag of 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with modified fuselage area distribution and faired inlet at Mach number from 0.82 to 1.68 : TED No. NACA DE 392 (open access)

Flight determination of minimum drag of 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with modified fuselage area distribution and faired inlet at Mach number from 0.82 to 1.68 : TED No. NACA DE 392

Report presenting a flight test conducted to determine the minimum drag of a 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with a transonic-area-rule fuselage-cross-sectional-area development. Results regarding the trim normal-force coefficient and measured drag are provided.
Date: September 26, 1955
Creator: Hastings, Earl C., Jr.
System: The UNT Digital Library
Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback (open access)

Flight Determination of the Longitudinal Stability and Control Characteristics of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback

Memorandum presenting the Bell X-5 research airplane tested at 58.7 degrees sweepback during the program to determine the characteristics of a variable-sweep fighter airplane at transonic speeds. This paper includes the stability and control characteristics in the stable lift range up to Mach numbers near 1.0 at an altitude of 40,000 feet and to slightly lower Mach numbers at altitudes of 25,000 feet and 15,000 feet. Results regarding general comments, static stability and control characteristics, and longitudinal dynamic stability are provided.
Date: May 26, 1955
Creator: Finch, Thomas W.
System: The UNT Digital Library
Preliminary Evaluation of Flight-Weight XRJ47-W-5 Ram-Jet Engine at a Mach Number of 2.75 (open access)

Preliminary Evaluation of Flight-Weight XRJ47-W-5 Ram-Jet Engine at a Mach Number of 2.75

Report presenting a free-jet investigation of the performance, burner-shell cooling, and ignition characteristics of a flight-weight 48-inch-diameter XRJ47-W-5 ramjet engine at an inlet Mach number of 2.75 and an angle of attack of 3 degrees. Data were obtained over a range of altitudes, inlet temperatures, and fuel-air ratios.
Date: July 26, 1955
Creator: Welna, Harry J. & Reilly, Dwight H.
System: The UNT Digital Library
Effects of Various Modifications on the Static Longitudinal Stability and Control Characteristics of a 0.065-Scale Model of the Chance Vought Regulus II Missile at a Mach Number of 2.01 (open access)

Effects of Various Modifications on the Static Longitudinal Stability and Control Characteristics of a 0.065-Scale Model of the Chance Vought Regulus II Missile at a Mach Number of 2.01

"An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects on the static longitudinal stability and control characteristics of various modifications to a 0.065-scale model of the Chance Vought Regulus II missile. The modifications consisted of a control housing on top of the fuselage, two sizes of canard surfaces with fixed incidence angles, various angles of nose droop, and two types of inlet boundary-layer bleed diverters. The tests were made at a Mach number of 2.01 and a Reynolds number, based on the mean aerodynamic chord of 1.54 x 10(exp 6)" (p. 1).
Date: September 26, 1955
Creator: Robinson, Ross B. & Driver, Cornelius
System: The UNT Digital Library
Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41 (open access)

Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41

Report presenting an investigation in the 4- by 4-foot supersonic pressure tunnel at a Mach number of 1.41 to determine the static stability and control and drag characteristics of a model of a 35 degree swept-wing airplane. The effects of alternate fuselage shapes, wing camber, wing fences, and fuselage dive brakes on aerodynamic characteristics were also investigated.
Date: May 26, 1955
Creator: Palazzo, Edward B. & Spearman, M. Leroy
System: The UNT Digital Library
Experimental Investigation at High Subsonic Speeds of the Rolling Stability Derivatives of a Complete Model with an Aspect-Ratio-2.52 Wing Having an Unswept 72-Percent-Chord Line and a High Horizontal tail (open access)

Experimental Investigation at High Subsonic Speeds of the Rolling Stability Derivatives of a Complete Model with an Aspect-Ratio-2.52 Wing Having an Unswept 72-Percent-Chord Line and a High Horizontal tail

Memorandum presenting rolling stability derivatives for a complete model with a low-aspect-ratio wing and tail surfaces for a Mach number range of 0.70 to 0.94 and for an angle-of-attack range from 0 to 13 degrees for the lower Mach numbers. The model test results indicated regions of neutral or unstable damping in roll at Mach numbers of 0.85 and 0.90 in the higher angle-of-attack range for the basic model. Results regarding damping in roll, yawing moment and lateral force due to rolling, and aileron characteristics are provided.
Date: May 26, 1955
Creator: Sleeman, William C., Jr. & Wiggins, James W.
System: The UNT Digital Library
Lateral stability and control characteristics of the Convair XF-92A delta-wing airplane as measured in flight (open access)

Lateral stability and control characteristics of the Convair XF-92A delta-wing airplane as measured in flight

Report presenting the lateral stability and control characteristics were investigated on the Convair XF-92A delta-wing airplane during the flights of the NACA research program. The investigation included sideslips, aileron rolls, and rudder pulses at a range of altitudes and indicated speeds. The lateral handling characteristics appear satisfactory when viewed in terms of gradually increasing sideslips, lateral control effectiveness, and period, and damping.
Date: May 26, 1955
Creator: Sisk, Thomas R. & Muhleman, Duane O.
System: The UNT Digital Library
Semi-Empirical Correlations of Alpha Decay Rates and Energies (open access)

Semi-Empirical Correlations of Alpha Decay Rates and Energies

None
Date: October 26, 1955
Creator: Gallagher, C. J., Jr. & Rasmussen, J. O.
System: The UNT Digital Library
HRT PROCESS FLOWSHEETS (open access)

HRT PROCESS FLOWSHEETS

None
Date: May 26, 1955
Creator: Zapp, F. C.
System: The UNT Digital Library
MEDICAL AND HEALTH PHYSICS QUARTERLY REPORT FOR APRIL, MAY, JUNE 1955 (open access)

MEDICAL AND HEALTH PHYSICS QUARTERLY REPORT FOR APRIL, MAY, JUNE 1955

None
Date: July 26, 1955
Creator: unknown
System: The UNT Digital Library
Metallex Dry-Salt Process Development Requirements (open access)

Metallex Dry-Salt Process Development Requirements

None
Date: July 26, 1955
Creator: Bresee, J. C. & Suddath, J. C.
System: The UNT Digital Library
[Imperial Sugar Company Estimated Daily Cash Balance: August 26, 1955] (open access)

[Imperial Sugar Company Estimated Daily Cash Balance: August 26, 1955]

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: August 26, 1955
Creator: Imperial Sugar Company
System: The Portal to Texas History
[Imperial Sugar Company Estimated Daily Cash Balance: August 26, 1955] (open access)

[Imperial Sugar Company Estimated Daily Cash Balance: August 26, 1955]

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: August 26, 1955
Creator: Imperial Sugar Company
System: The Portal to Texas History
[Invoice for Cattle Account, April 26, 1955] (open access)

[Invoice for Cattle Account, April 26, 1955]

Invoice for items sold for Sugarland Industries by the Live Stock Commission Company, including the pricing and amount of cattle sold.
Date: April 26, 1955
Creator: C. B. Johnson Live Stock Commission Company
System: The Portal to Texas History
[Invoice for Cattle Account, April 26, 1955] (open access)

[Invoice for Cattle Account, April 26, 1955]

Invoice for items sold for Sugarland Industries by the Live Stock Commission Company, including the pricing and amount of cattle sold.
Date: April 26, 1955
Creator: C. B. Johnson Live Stock Commission Company
System: The Portal to Texas History