Resource Type

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Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future) (open access)

Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future)

From Summary: "This report presents a compilation of static sea-level data on existing or designed American and British axial-flow turbojet engines in terms of basic engine parameters such as thrust and air flow. In the data presented, changes in the over-U engine performance with time are examined as well as the relation of the various engine parameters to each other."
Date: December 10, 1951
Creator: Cesaro, Richard S. & Lazar, James
System: The UNT Digital Library
Report of the Thirty-Sixth National Conference on Weights and Measures, 1951 (open access)

Report of the Thirty-Sixth National Conference on Weights and Measures, 1951

Report of the annual conference on weights and measures, hosted by the U.S. National Bureau of Standards in Washington D.C. It includes conference proceedings, a list of attendees, information about committees and officers, and other reports or commentaries discussed at the meetings.
Date: December 10, 1951
Creator: United States. National Bureau of Standards.
System: The UNT Digital Library
Over-all performance of J35-A-23 two-stage turbine (open access)

Over-all performance of J35-A-23 two-stage turbine

Over-all performance of a two-stage turbine from a J35-A-23 turbojet engine is presented. Limiting blade loading restricted work output to approximately 95 percent of the design value. The brake internal efficiency at design operating conditions was approximately 0.75. maximum brake internal efficiency at off-design conditions was between 0.81 and 0.82.
Date: December 10, 1951
Creator: Rebeske, John J., Jr.; Berkey, William E. & Forrette, Robert E.
System: The UNT Digital Library
Damping in Roll of Straight and 45 Degree Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds With Rocket-Powered Models (open access)

Damping in Roll of Straight and 45 Degree Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds With Rocket-Powered Models

Report presenting rocket-powered flight testing to determine the damping in roll of several wings of 0 degree and 45 degree quarter-chord-line sweep with various taper ratios for a range of Mach numbers. Damping in roll decreased with decreasing taper ratio at roughly the same rate for swept and unswept wings and also decreased by sweeping the quarter-chord line. The experimental results were also consistently lower than what was predicted by theory.
Date: October 10, 1951
Creator: Sanders, E. Claude, Jr.
System: The UNT Digital Library
Homogeneous Reactor Project Quarterly Progress Report [for] Period Ending May 15, 1951 (open access)

Homogeneous Reactor Project Quarterly Progress Report [for] Period Ending May 15, 1951

Technical report outlining the reconstitution of the Homogeneous Reactor Experiment Project (HRE) as the Homogeneous Reactor Project. Report covers the need for a broader developmental program to establish the feasibility of obtaining the potential advantages of homogeneous reactors for the production of fissionable materials and power. Details the ultimate objective of the ORNL program to provide the technical information required to determine the feasibility of a full scale plutonium power producing homogeneous reactor. [From Summary]
Date: October 10, 1951
Creator: Swartout, J. A.; Secoy, C. H. & Winters, C. E.
System: The UNT Digital Library
Preliminary Investigation of the Effects of Rectangular Vortex Generators on the Performance of a Short 1.9:1 Straight-Wall Annular Diffuser (open access)

Preliminary Investigation of the Effects of Rectangular Vortex Generators on the Performance of a Short 1.9:1 Straight-Wall Annular Diffuser

Report presenting a preliminary investigation in a duct system with fully developed pipe flow to determine the effectiveness of vortex generators in improving the performance of a 21-inch-diameter straight-outer-wall annual diffuser with an overall equivalent conical expansion angle of 15 degrees and a and 1.9:1 area ratio. The vortex generators used were rectangular noncambered airfoils that varied in chord, span, angle of attack, number, and location. Results regarding a diffuser with no vortex generators, a diffuser with vortex generators on inner body, and a comparison of the diffuser performance with and without vortex generators are provided.
Date: October 10, 1951
Creator: Wood, Charles C.
System: The UNT Digital Library
Experimental Study of the Effect of Sweepback on Transonic Aileron Flutter (open access)

Experimental Study of the Effect of Sweepback on Transonic Aileron Flutter

Report presenting the effects of sweepback on the occurrence and principal characteristics of single-degree-of-freedom aileron flutter for a wing-aileron combination. Testing occurred over a range of Mach and Reynolds number and angles of attack. Results regarding the measurements of aileron motion, effect of sweep, variation of lift coefficient, and use of shadowgraph technique for visualizing flow are provided.
Date: September 10, 1951
Creator: Levy, Lionel L., Jr. & Knechtel, Earl D.
System: The UNT Digital Library
Leaching and Precipitation Tests on Grants Ores (open access)

Leaching and Precipitation Tests on Grants Ores

Leaching tests were run on two samples from the Grants area in New Mexico. Uranium extractions of 94 per cent were obtained by leaching Sample 6-1 with solutions containing 240 lbs. of Na2CO3 and 60 lbs. of NaHCO3 per ton and by leaching Sample 6-2 with 270 lbs. of Na2CO3 and 180 lbs. of NaHCO3 per ton. Cyclic tests were completed using caustic precipitation of the leach liquor.
Date: September 10, 1951
Creator: Abrams, Charles S. & George, D'Arcy R.
System: The UNT Digital Library
Low-Speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-Wing: Fuselage Combination at a Reynolds Number of 6.0 X 10(Exp 6) (open access)

Low-Speed Investigation of the Effects of Single Slotted and Double Slotted Flaps on a 47.7 Degree Sweptback-Wing: Fuselage Combination at a Reynolds Number of 6.0 X 10(Exp 6)

Report presenting an investigation to determine the effects of partial-span single slotted and double slotted flaps at various deflections on the longitudinal aerodynamic characteristics of a sweptback-wing-fuselage combination. Results regarding the lift characteristics, pitching-moment characteristics, drag characteristics, and effect of flap-bracket alignment are provided.
Date: September 10, 1951
Creator: Mollenberg, Ernst F. & Spooner, Stanley H.
System: The UNT Digital Library
Removal of ruptured slug from tube No. 2068-H (open access)

Removal of ruptured slug from tube No. 2068-H

None
Date: September 10, 1951
Creator: unknown
System: The UNT Digital Library
RM line equipment problems associated with a proposed increase in batch size (open access)

RM line equipment problems associated with a proposed increase in batch size

The effect made on the RM (Remote Mechanical) Line equipment by an increase in the plant batch size from ca. 300 grams to ca. 375 grams has been studied. Using the process as determined by Production Test 234-3, the volumes for a 300 gram batch and a 375 gram batch are as follows, respectively: volume of plutonium peroxide (alcohol washed, filtered)--1,275 cc., 1,593 cc.; volume of plutonium tetrafluoride (as produced)--617.7 cc., 772 cc.; and volume of reduction charge (tamped)--511 cc., 638 cc. The difficulties encountered with 375 gram batches are discussed.
Date: September 10, 1951
Creator: Quinn, F. J., Jr.
System: The UNT Digital Library
The Synthetic Liquid Fuel Potential of Wyoming/Idaho (open access)

The Synthetic Liquid Fuel Potential of Wyoming/Idaho

Report documenting the suitability of Wyoming and Idaho for plant locations to produce synthetic liquid fuels, based on raw materials, water sources, and local interest.
Date: September 10, 1951
Creator: Ford, Bacon, and Davis
System: The UNT Digital Library
The Argonne Heavy Water Reactor (CP-3 Prime) (open access)

The Argonne Heavy Water Reactor (CP-3 Prime)

The following document provides figures with all information that describe the heavy water moderated chain reacting pile at Argonne National Laboratory.
Date: August 10, 1951
Creator: Zinn, Walter H.
System: The UNT Digital Library
The Synthetic Liquid Fuel Potential of North Dakota and South Dakota (open access)

The Synthetic Liquid Fuel Potential of North Dakota and South Dakota

Report documenting the suitability of North Dakota and South Dakota for plant locations to produce synthetic liquid fuels, based on raw materials, water sources, and local interest...add details/adjust
Date: August 10, 1951
Creator: Ford, Bacon, and Davis
System: The UNT Digital Library
Compilation and review of effects of design parameters on ditching characteristics (open access)

Compilation and review of effects of design parameters on ditching characteristics

From Summary: "This paper supplements a previously published one on the effect of design parameters on ditching characteristics. The supplementary information is based on additional data available from both model tests and full-scale experience. In addition, summary tables compiled from the NACA model ditching investigations are presented."
Date: July 10, 1951
Creator: Fisher, Lloyd J. & Hoffman, Edward L.
System: The UNT Digital Library
Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method (open access)

Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method

Report presenting an aerodynamic investigation in the high-speed 7- by 10-foot tunnel to determine the effects of taper-in-thickness on the aerodynamic characteristics of wings with 35 and 45 degrees of sweepback, aspect ratio 6, and taper ratio 0.60. The wings were tested over a range of Mach numbers.
Date: July 10, 1951
Creator: Morrison, William D., Jr. & Fournier, Paul G.
System: The UNT Digital Library
Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails (open access)

Free-Flight Investigation of the Longitudinal Stability and Control of a Rocket-Propelled Missile Model Having Cruciform, Triangular, Interdigitated Wings and Tails

Report presenting flight testing of a missile model with cruciform, triangular, interdigitated wings and tails to determine the longitudinal stability and control characteristics over a range of Mach numbers. Results regarding static stability and damping, control effectiveness, and control hinge moments are provided.
Date: July 10, 1951
Creator: Sandahl, Carl A. & Hall, James R.
System: The UNT Digital Library
Graphite Sample Boring from Process Channels : Final Report, Production Test 105-389-P (open access)

Graphite Sample Boring from Process Channels : Final Report, Production Test 105-389-P

The following report records a total of forty-nine graphite core samples that have been bored from process tube blocks in the Hanford piles with the intention to provide results to indicate that core boring is an entirely practical operation over bore scraping in obtaining powder samples.
Date: July 10, 1951
Creator: Cole, J. B.
System: The UNT Digital Library
Graphite Sample Boring from Process Channels : Final Report, Production Test 105-389-P (open access)

Graphite Sample Boring from Process Channels : Final Report, Production Test 105-389-P

The following report records a total of forty-nine graphite core samples that have been bored from process tube blocks in the Hanford piles with the intention to provide results to indicate that core boring is an entirely practical operation over bore scraping in obtaining powder samples.
Date: July 10, 1951
Creator: Cole, J. B.
System: The UNT Digital Library
Low-Speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-Wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X 10(Exp 6) (open access)

Low-Speed Investigation of Several Types of Split Flap on a 47.7 Degree Sweptback-Wing - Fuselage Combination of Aspect Ratio 5.1 at a Reynolds Number of 6.0 X 10(Exp 6)

Report presenting a low-speed wind-tunnel investigation to determine the longitudinal aerodynamic characteristics of a 47.7 degree sweptback wing-fuselage combination with split flaps and several modifications. The lift characteristics, pitching-moment characteristics, drag characteristics, and a comparison with flaps of the slotted type are included.
Date: July 10, 1951
Creator: Spooner, Stanley H. & Mollenberg, Ernst F.
System: The UNT Digital Library
Pile modification resulting in increased power levels (open access)

Pile modification resulting in increased power levels

The power output of the piles is being restricted primarily by three important limitations; those due to graphite temperatures, slug and tube corrosion and maximum power per tube or ``boiling disease.`` The purpose of this document is to present means for increasing very appreciably the ``boiling disease`` limits. In addition, means for alleviating the corrosion limitations will be discussed.
Date: July 10, 1951
Creator: Carbon, M. W. & Fryar, R. M.
System: The UNT Digital Library
Production Test 105-389-P graphite sample boring from process channels. Final report (open access)

Production Test 105-389-P graphite sample boring from process channels. Final report

The study of radiation damage to the graphite moderator is largely dependent upon the availability of graphite samples from the moderator itself. Because of the varied temperature-flux history and complicated structure of the piles, it is impossible to study the problem from the laboratory standpoint alone. The samples of greatest interest are those taken from the sections of the moderator which have received the greatest damage. However, a comprehensive study requires samples from all sections of the graphite moderator. It is desirable that these samples be solid in order that physical and dimensional measurements of all types may be made. Solid samples enable thermal conductivity measurements and the gradients of damage across tube blocks to be measured. To provide such samples, it was necessary to design some device which would cut solid samples from any location in the pile through the process Channels. The graphite core borer was desigred specifically for this purpose. The objective of this Production Test was to test the operation of the core barer and evaluate the results of its performance.
Date: July 10, 1951
Creator: Cole, J. B.
System: The UNT Digital Library
Recommendations for slug improvement (open access)

Recommendations for slug improvement

None
Date: July 10, 1951
Creator: Burnham, J. B., Jr.
System: The UNT Digital Library
A Solvent Extraction Method for Neptunium (237) Analysis (open access)

A Solvent Extraction Method for Neptunium (237) Analysis

Technical report describing a rapid and quantitative radiochemical method for the analysis of neptunium (237). This method is based on the extraction of neptunium (IV) with thenoyl-trifluoracetone in xylene. Neptunium (237) is separated free from other alpha emitters and from non-radioactive interferences, and the method may be readily adapted to remote control. [From Abstract]
Date: July 10, 1951
Creator: Moore, Fletcher L.
System: The UNT Digital Library