Comparison of Free-Flight Measurements of the Zero-Lift Drag Rise of Six Airplane Configurations and Their Equivalent Bodies of Revolution at Transonic Speeds (open access)

Comparison of Free-Flight Measurements of the Zero-Lift Drag Rise of Six Airplane Configurations and Their Equivalent Bodies of Revolution at Transonic Speeds

"Free-flight drag measurements are presented which show the practicability of duplicating the zero-lift drag rise of many airplane configurations by simple bodies of revolution. The results confirm the transonic area rule for straight wings, and for delta and modified-delta wings with and without nacelles. The results showed that the area rule did not apply to one swept-wing configuration and an explanation is advanced to explain why it does not apply" (p. 1).
Date: January 5, 1954
Creator: Hall, James Rudyard
System: The UNT Digital Library
Flight determined buffet boundaries of ten airplanes and comparisons with five buffeting criteria (open access)

Flight determined buffet boundaries of ten airplanes and comparisons with five buffeting criteria

Report presenting the flight-determined buffet boundaries of ten airplanes. Comparisons are made with five possible buffeting criteria related to airfoil-section characteristics. The primary factors that determine buffeting criteria are critical Mach number, Mach number of sonic flow at the crest, lift-divergence Mach number, lift-peak Mach number, and empirical buffeting criterion are provided.
Date: January 5, 1951
Creator: Gadeberg, Burnett L. & Ziff, Howard L.
System: The UNT Digital Library
Load-Range Performance of Turbine-Propeller Engine in Transonic Speed Range and Comparison With Load-Range Performance of Turbojet Engine (open access)

Load-Range Performance of Turbine-Propeller Engine in Transonic Speed Range and Comparison With Load-Range Performance of Turbojet Engine

Memorandum presenting an investigation of the effect on load-range performance of various combinations of compressor pressure ratio and turbine-inlet temperature for the turbine-propeller engine and to provide a means for comparing the load range of turbine-propeller and turbojet engines for a range of flight speeds.
Date: January 5, 1951
Creator: Lubarsky, Bernard
System: The UNT Digital Library
The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing (open access)

The effects of boundary-layer control on the longitudinal characteristics of a swept-back wing using suction through streamwise slots in the outboard portion of the wing

Report presenting an investigation to determine the effects of a simplified form of boundary-layer control on the low-speed longitudinal characteristics of a sweptback wing. The primary objective was to improve the longitudinal characteristics of the sweptback wing at lift coefficients below the maximum. Results regarding the characteristics of the wing without boundary-layer control and effects of boundary-layer control are provided.
Date: January 5, 1951
Creator: McCormack, Gerald M. & Tolhurst, William H., Jr.
System: The UNT Digital Library
Laminar mixing of a compressible fluid (open access)

Laminar mixing of a compressible fluid

From Summary: "A theoretical investigation of the velocity profiles for laminar mixing of a high-velocity stream with a region of fluid at rest has been made assuming that the Prandtl number is unity. A method which involves only quadratures is presented for calculating the velocity profile in the mixing layer for an arbitrary value of the free-stream Mach number. Detailed velocity profiles have been calculated for free-stream Mach numbers of 0, 1, 2, 3, and 5."
Date: January 5, 1949
Creator: Chapman, Dean R.
System: The UNT Digital Library
Tests of the Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Wing Modifications (open access)

Tests of the Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Wing Modifications

"Wind-tunnel tests were conducted to determine the longitudinal stability characteristics of a full-scale Northrop XSSM-A-3 missile. Various wing modifications were investigated in an effort to provide a configuration that would maintain longitudinal stability to lift coefficients necessary for landing the missile during flight tests. The results of the tests led to the choice of a wing with an increased leading-edge radius" (p. 1).
Date: January 5, 1950
Creator: Graham, David
System: The UNT Digital Library
Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 2 - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 Degrees (open access)

Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 2 - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 Degrees

The stator-blade angles in the twelfth through fifteenth stages of a 16-stage axial-flow compressor were increased 3O. The over-all performance of this modified compressor is compared to the performance of the compressor with original blade angles. The matching characteristics of the modified compressor and a two-stage turbine were obtained and compared to those of the compressor with original blade angles and the same turbine.
Date: January 5, 1952
Creator: Hatch, James E. & Medeiros, Arthur A.
System: The UNT Digital Library
The Influence of Exhaust Pressure on Knock-Limited Performance (open access)

The Influence of Exhaust Pressure on Knock-Limited Performance

Report discussing testing on two types of single cylinders to determine the effect of the relation of exhaust pressure to inlet-air pressure on knock-limited performance. Variables explored included exhaust pressure, fuel-air ratio, and engine speed. Three types of fuels were also used to explore the effect of exhaust pressure on fuel ratings.
Date: January 5, 1945
Creator: Cook, Harvey A.; Held, Louis F. & Pritchard, Ernest I.
System: The UNT Digital Library
Low-Speed Investigation of the Effects of Location of a Delta and a Straight Tail on the Longitudinal Stability and Control of a Thin Delta Wing With Extended Double Slotted Flaps (open access)

Low-Speed Investigation of the Effects of Location of a Delta and a Straight Tail on the Longitudinal Stability and Control of a Thin Delta Wing With Extended Double Slotted Flaps

Report presenting an investigation to determine the effects of horizontal-tail location and plan form on the longitudinal stability and control characteristics of a fuselage and thin delta wing with extended double slotted flaps. Several configurations of the aircraft, including flaps with the tail off, extended double slotted flaps, and canard with extended double slotted flap and delta tail are explored.
Date: January 5, 1954
Creator: Riebe, John M. & Graven, Jean C., Jr.
System: The UNT Digital Library
Effect on Transonic and Supersonic Drag of a Fuselage Protuberance of an Essential Unswept Wing-Fuselage Combination (open access)

Effect on Transonic and Supersonic Drag of a Fuselage Protuberance of an Essential Unswept Wing-Fuselage Combination

"An investigation of the effect on transonic and supersonic drag of a fuselage protuberance designed to improve the overall longitudinal distribution of cross-sectional area of an essentially unswept wing-fuselage combination has been made with free-flight rocket models. The wing-fuselage configuration was tested with and without a fuselage protuberance designed to relieve the steep area gradient over the rear portion of the wing" (p. 1).
Date: January 5, 1954
Creator: Sandahl, Carl A.
System: The UNT Digital Library
A cascade-general-momentum theory of operation of a supersonic propeller annulus (open access)

A cascade-general-momentum theory of operation of a supersonic propeller annulus

Report presenting a cascade-general-momentum theory method for calculating the operating conditions of a supersonic propeller annulus throughout the flight Mach number range. General flow patterns about the cascade and adjustments to free-stream conditions are discussed.
Date: January 5, 1953
Creator: Klawans, Bernard B. & Vogeley, Arthur W.
System: The UNT Digital Library
A Miniature Mixer Settler (open access)

A Miniature Mixer Settler

Unit developed at Knolls Atomic Power Laboratory for extraction and overcomes the disadvantages of the batch countercurrent units currently in use.
Date: January 5, 1956
Creator: Alter, H. Ward; Coplan, B. V. & Zebroski, E. L.
System: The UNT Digital Library
High Power Density Development Project: Interim Report, 300 MWe HPD Conceptual Design Study (open access)

High Power Density Development Project: Interim Report, 300 MWe HPD Conceptual Design Study

From introduction: "Preliminary design and analysis of the 300 MWe core."
Date: January 5, 1962
Creator: Grayhek, V. G.
System: The UNT Digital Library
Facilities, National Institute of Standards and Technology (open access)

Facilities, National Institute of Standards and Technology

From page 2: The National Institute of Standards and Technology research reactor is a national center for the application of reactor radiation to a variety of problems of national concern. Major program areas at the reactor include the application of neutron scattering methods to research in materials science, trace analysis by neutron activation, nondestructive evaluation (via neutron radiography and scattering), neutron standards and dosimetry , and isotope production and radiation effects.
Date: January 5, 1989
Creator: National Institute of Standards and Technology (U.S.)
System: The UNT Digital Library
A Study of the Feasibility of Using Scintillating Fibers for Low Energy Beta Counting: Quarterly Report Number 1, June - September 1961 (open access)

A Study of the Feasibility of Using Scintillating Fibers for Low Energy Beta Counting: Quarterly Report Number 1, June - September 1961

From introduction: "A detector system with the advantages of a liquid counter, but without the severe requirements on sample preparations, has been devised and is the basis of the present experimental investigation."
Date: January 5, 1962
Creator: Preston, C.
System: The UNT Digital Library
Improved Zirconium Alloys : Ninth Monthly Report Covering the Period December 1 to December 31, 1960 (open access)

Improved Zirconium Alloys : Ninth Monthly Report Covering the Period December 1 to December 31, 1960

The following report is the ninth in a series of monthly reports covering the program with the objective of developing alloys having superior 680 F water and/or 750 to 900 F steam corrosion resistance, as well as developing higher strength alloys for current temperature ranges while still maintaining corrosion resistance comparable to that of Zircaloy-2. This report was made covering the period December 1 to December 31, 1960.
Date: January 5, 1961
Creator: Weinstein, Daniel & Van Thyne, R. J.
System: The UNT Digital Library
Interim Report on Examination of Powder Metallurgy Slug from PT-105-313-4M (open access)

Interim Report on Examination of Powder Metallurgy Slug from PT-105-313-4M

This report examines a uranium slug that has been produced by powder metallurgical methods and exposed in the 100-DR Pile and was deformed during pile exposure.
Date: January 5, 1953
Creator: O'Keefe, D. P.
System: The UNT Digital Library
Analysis of Lid Tank Neutron Data for Lead and Iron (open access)

Analysis of Lid Tank Neutron Data for Lead and Iron

Abstract: An analysis of the lid tank neutron data for Pb-H2O and Fe-H2O is made. "Effective" fast neutron cross sections for the metals are obtained. This is based on the "one collision theory" of shielding. Values are 3.4 barns for Pb and 2.0 barns for Fe. These compare very well with those obtained by Albert and Welton based on other lid tank data and another method of calculation.
Date: January 5, 1951
Creator: Podgor, S.
System: The UNT Digital Library
Preparation of Thin, Self-supporting Copper Films (open access)

Preparation of Thin, Self-supporting Copper Films

A repeatable technique for preparation of thin, self-supporting copper films has been developed at the Lawrence Radiation Laboratory in Livermore, California. The process, done in a vacuum chamber, involves evaporation of copper by electron bombardment, and deposition of the copper on a detergent-coast glass substrate. The copper film is later removed from the substrate by immersion in water.
Date: January 5, 1961
Creator: Brunner, W. & Patton, H.
System: The UNT Digital Library
Removal of Deuterated Boric Acid From Deuterium Oxide Solution by Ion Exchange Resin (open access)

Removal of Deuterated Boric Acid From Deuterium Oxide Solution by Ion Exchange Resin

Introduction: "Because of the importance of the value of the transport mean free path of thermal neutrons in deuterium oxide, Kash and Woods proposed to redetermine this value in deuterium oxide (99.4 atom-percent deuterium, by an extrapolation method. Kash and Woods thought that the low value of the transport mean free path might be a source of error. This paper relates studies of procedures by which (1) boron material would be dissolved in high content deuterium oxide without adding foreign atoms, particularly hydrogen atoms which might adversely affect the test, (2) the boron content of the deuterium oxide solvent may be determined, (3) ion exchangers may be deuterized and de-deuterized, and (4) ion exchange may remove specific ions from solution."
Date: January 5, 1954
Creator: Silverman, L.
System: The UNT Digital Library
An Abrasive Cutoff Machine for Metallurgical Research on Radioactive Materials (open access)

An Abrasive Cutoff Machine for Metallurgical Research on Radioactive Materials

An abrasive cutoff machine design, based upon a previous model, (1) was undertaken to provide for the sampling of radioactive material. the design objective was; first, to provide samples for metallographic examination, second, to provide samples for physical and mechanical property testing, and, third, to meet the following design requirements: 1. Remote operation. 2. Airborne contamination control. 3. Radioactive waste collection. 4. Remote maintenance.
Date: January 5, 1957
Creator: Boyd, C. L.
System: The UNT Digital Library
A Transistorized GM Survey Instrument (open access)

A Transistorized GM Survey Instrument

A portable GM survey instrument was designed and developed which consists of a single transistor blocking-oscillator high voltage supply, a dual transistor multivibrator count-rate meter and a standard 30 mg/cm² glass-wall GM tube.
Date: January 5, 1956
Creator: Spear, W. G.
System: The UNT Digital Library
Beam Current Integrator (open access)

Beam Current Integrator

The object of this report is to acquaint the operator with the operational and technical aspects of the beam current integrator as well as the theory of the system operation. The design and operation of a beam current integrator are described, and the theory of operation is discussed. The instrument has two channels. The console channel is designed to measure the accumulation of charge received by a target during a period of a day no matter what the range used in the experimenter's channel. An analysis indicated that this unit will measure the accumulation of charge by a target to an accuracy of 0.1215% assuming that the constant error due to shorting the integrating capacitor is accounted for. The instrument is ranged to handle from 0.5 to 500 mu a of beam current. (M.C.G.)
Date: January 5, 1962
Creator: Jacobs, J.
System: The UNT Digital Library
Homogeneous Reactor Test Summary Report for the Advisory Committee on Reactor Safeguards (open access)

Homogeneous Reactor Test Summary Report for the Advisory Committee on Reactor Safeguards

The Homogeneous Reactor Test (HRT) is the experimental reactor facility (Frontispiece) being designed and constructed at ORNL as the next step in homogeneous reactor development between the 1-Mv HRE and a "full-scale" power station. The HRT will provide an integrated test at 5 to 10 Mv for the flowsheet and equipment designs on which the full-scale effort will be based. Furthermore, its design is such that several homogeneous systems which require essentially the same operating equipment may be tested with comparatively minor modifications of the original reactor installation. The reactor will be assembled in the building which housed the HRE, located in the experimental reactor exclusion area approximately one mile south of the oak ridge laboratory. (See figure 1) / It is the purpose of this report to provide information with which the hazardous aspects of this reactor may be evaluated. Briefly, it will be shown after a statement of purpose and a general description of the reactor that: 1. The design characteristics and equipment requirements are such that escape of highly reactive material from the reactor piping is unlikely. 2. Should the entire core and blanket contents suddenly escape from the reactor system, a seal-welded steel tank surrounding the …
Date: January 5, 1955
Creator: Beall, S. E. & Visner, S.
System: The UNT Digital Library