Resource Type

States

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers Up to 0.87 (open access)

Flight Measurements With the Douglas D-558-II (BuAero No. 37974) Research Airplane: Static Lateral and Directional Stability Characteristics as Measured in Sideslips at Mach Numbers Up to 0.87

Report presenting flight measurements in sideslips of the static lateral and directional stability characteristics of the Douglas D-558-II airplane. It is part of an investigation to determine the stability and control characteristics and aerodynamic loads acting on the wing and horizontal tail of an airplane from stalling speed up to a maximum Mach number of 0.90. Results regarding variations of rudder, total aileron, elevator control positions and control forces, aileron position, and aerodynamic hinge moments are provided.
Date: May 19, 1950
Creator: Sjoberg, S. A.
Object Type: Report
System: The UNT Digital Library
Interim Memorandum Report on Filter Development and Discussion on Availability of Materials (open access)

Interim Memorandum Report on Filter Development and Discussion on Availability of Materials

None
Date: May 19, 1950
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Wind-tunnel investigation at low speed to determine aerodynamic properties of a jettisonable nose section with circular cross section (open access)

Wind-tunnel investigation at low speed to determine aerodynamic properties of a jettisonable nose section with circular cross section

Report presenting the aerodynamic properties of a model of a jettisonable nose section with a circular cross section as determined at low speed from an investigation in the 20-foot free-spinning tunnel. The results indicated that the aerodynamic characteristics of the nose were greatly affected by proximity to the fuselage. Even for a stabilized nose, it may be necessary to eject the nose forward forcibly in order to prevent high accelerations along the backbone of the pilot.
Date: May 19, 1950
Creator: Goodwin, Roscoe H.
Object Type: Report
System: The UNT Digital Library
Aerodynamic Loading Characteristics of a Wing-Fuselage Combination Having a Wing of 45 Degrees Sweepback Measured in the Langley 8-Foot Transonic Tunnel (open access)

Aerodynamic Loading Characteristics of a Wing-Fuselage Combination Having a Wing of 45 Degrees Sweepback Measured in the Langley 8-Foot Transonic Tunnel

Report presenting an investigation of the aerodynamic loading characteristics of a wing-fuselage combination in the slotted test section of the transonic tunnel. The test was part of a systematic investigation of the effects of varying the amount of sweepback on wings in order to determine their suitability for transonic flight. Results regarding span load characteristics, normal-force characteristics, wing-tip angle of twist, spanwise distribution of section pitching-moment coefficient, pitching-moment characteristics, and fuselage characteristics in presence of wing are provided.
Date: May 19, 1952
Creator: Loving, Donald L. & Williams, Claude V.
Object Type: Report
System: The UNT Digital Library
Critical mass studies of plutonium solutions (open access)

Critical mass studies of plutonium solutions

The chain reacting conditions for plutonium nitrate in water solution have been examined experimentally for a variety of sizes of spheres and cylinders. The effects on the critical mass of the displacement of hydrogen and the addition of poisons to the fuel were measured in water tamped and bare reactors. In this report the data obtained in the investigation is presented graphically and in tables. Some preliminary analysis has been made yielding the results: (i) the absorption cross-section of Pu{sup 240} is 925 {plus_minus} 200 barns and (ii) the minimum critical mass of Pu{sup 239} in water is 510 grams at concentration of about 33 grams per liter.
Date: May 19, 1952
Creator: Kruesi, F. E.; Erkman, J. O. & Lanning, D. D.
Object Type: Report
System: The UNT Digital Library
Normal Accelerations and Associated Operating Conditions on Four Types of Commercial Transport Airplanes From VGH Data Available as of September 1951 (open access)

Normal Accelerations and Associated Operating Conditions on Four Types of Commercial Transport Airplanes From VGH Data Available as of September 1951

Memorandum presenting results obtained from time-history records of normal accelerations, airspeed, and altitude. Additional data have been obtained from the operations of two types of commercial transport airplanes together with data on two other types of transport airplanes.
Date: May 19, 1952
Creator: Steiner, Roy & Persh, Doris A.
Object Type: Report
System: The UNT Digital Library
Preliminary evaluation of Pennsalt A-10 and Turco ``Aviation`` Cleaner for cleaning aluminum caps and cans (open access)

Preliminary evaluation of Pennsalt A-10 and Turco ``Aviation`` Cleaner for cleaning aluminum caps and cans

The Process Unit has requested the Present Canning group to evaluate two alkaline cleaners, Pennsalt A-10 and Turco ``Aviation`` Cleaner, as possible substitutes for the present trichloroethylene vapor degreaser and Duponol wash. Disadvantages of the present cleaning procedure are: ineffectiveness; expense; toxicity of trichloroethylene. The alkaline cleaners Pennsalt A-10 and Turco ``Activation`` Cleaner were tested and compared with an alkaline cleaner made from Na{sub 2}CO{sub 3} and Na{sub 3}PO{sub 4} and with the present cleaning method. With available equipment Pennsalt A-10 and Turco ``Aviation`` Cleaner did not remove grease and dirt as well as the present cleaning method. A solution of Na{sub 2}PO{sub 4} and Na{sub 2}CO{sub 3} was the best degreaser tested although it did etch the surface of the cap. This document provides a discussion of the procedure utilized and the results.
Date: May 19, 1952
Creator: Weakley, E. A.
Object Type: Report
System: The UNT Digital Library
Use of an Aerodynamically Pulsed All-Movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-Powered Models in Free Flight and Some Initial Results From an Arrow-Wing-Body-Tail Configuration (open access)

Use of an Aerodynamically Pulsed All-Movable Horizontal Tail to Obtain Longitudinal Characteristics of Rocket-Powered Models in Free Flight and Some Initial Results From an Arrow-Wing-Body-Tail Configuration

Report presenting the application of an aerodynamically pulsed horizontal tail to determine experimentally the longitudinal aerodynamic characteristics of a rocket-powered model in free flight. Results regarding time history, lift and drag, and tail effectiveness and downwash are provided.
Date: May 19, 1952
Creator: Gillespie, Warren, Jr. & Dietz, Albert E.
Object Type: Report
System: The UNT Digital Library
Full Scale 48 MC Cavity For Sparking Tests of Gaps Corresponding to 0.45 To 4.5 Mev Beam Energy (open access)

Full Scale 48 MC Cavity For Sparking Tests of Gaps Corresponding to 0.45 To 4.5 Mev Beam Energy

It is proposed to test gaps corresponding to deuteron energies in the range of 0.45 to 4.5 Mev. The accelerator to be modeled is a 48 mc/sec cylindrical cavity in the TM010 mode with [formula] repeat length, [formula] gap, 0.25 megavolt per cavity foot peak r.f. gradient and strong focusing magnets alternating polarity at each drift tube.
Date: May 19, 1953
Creator: Unnam, Craig S.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: MS-37 (open access)

Texas Attorney General Opinion: MS-37

Letter opinion issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: The authority of the Board of Insurance Commissioners to reduce fire insurance rates in cities which have contracts with other municipalities for fire fighting services.
Date: May 19, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-43 (open access)

Texas Attorney General Opinion: S-43

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification: Several questions relating to the amount of securities which must be pledged by the county depository.
Date: May 19, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-131 (open access)

Texas Attorney General Opinion: MS-131

Letter opinion issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, John Ben Shepperd, regarding a legal question submitted for clarification; Disposition of tax revenue collected under Art. 881a-6, V.C.S.
Date: May 19, 1954
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
APPR critical experiment program meeting (open access)

APPR critical experiment program meeting

This report addresses the APPR critical experiment program meeting.
Date: May 19, 1955
Creator: Gallagher, J G
Object Type: Report
System: The UNT Digital Library
CALCULATION OF THE VOLUME OF LIQUID CONTAINED IN A PARTIALLY-FILLED RIGHT CIRCULAR CYLINDER INCLINED TO THE HORIZONTAL (open access)

CALCULATION OF THE VOLUME OF LIQUID CONTAINED IN A PARTIALLY-FILLED RIGHT CIRCULAR CYLINDER INCLINED TO THE HORIZONTAL

None
Date: May 19, 1955
Creator: Tobias, M
Object Type: Report
System: The UNT Digital Library
Low-Melting Alloys for Cast Fuel Elements (open access)

Low-Melting Alloys for Cast Fuel Elements

The following report follows an investigation made to determine the composition of uranium-rich ternary eutectic alloys most suitable for reactor application in the as-cast condition. These determinations were made based metallographic examination and thermal analysis of as-cast alloys.
Date: May 19, 1955
Creator: Saller, Henry A.; Rough, Frank A. & Bauer, Arthur A.
Object Type: Report
System: The UNT Digital Library
THE STABILITY OF THE RARE EARTH COMPLEXES WITH N- HYDROXYETHYLETHYLENEDIAMINETRIACETIC ACID (open access)

THE STABILITY OF THE RARE EARTH COMPLEXES WITH N- HYDROXYETHYLETHYLENEDIAMINETRIACETIC ACID

None
Date: May 19, 1955
Creator: Spedding, F. H.; Powell, J. E. & Wheelwright, E. J.
Object Type: Report
System: The UNT Digital Library
A Study of the Fabrication Failures for Zirconium and Zircaloy-2 Process Tubes and of the Annealing and Cold Rolling of Zircaloy-2 (open access)

A Study of the Fabrication Failures for Zirconium and Zircaloy-2 Process Tubes and of the Annealing and Cold Rolling of Zircaloy-2

A study of the fabrication failures for zirconium and zircaloy-2 process tubes was made. In the tube reducing operation, a non-uniform reduction in area for the cross section was found to be a major cause of failure. In annealing studies, a cycle of 2 hours at 820 deg C in vacuum followed by furnace cooling produced the greatest ductility of extruded zircaloy-2 for the annealing treatments studied. The ductility of cold worked and annealed zircaloy-2 was found to be superior to that of extruded and annealed material. The strain rate of a cold working process was found to affect the ductility of zircaloy-2.
Date: May 19, 1955
Creator: Johnson, Dale E.
Object Type: Report
System: The UNT Digital Library
Direct Interaction Neutrons From 14-MeV Inelastic Neutron Scattering (open access)

Direct Interaction Neutrons From 14-MeV Inelastic Neutron Scattering

BS>Neutron nonelastic cross sections measurcd at different detector biases have been used to determine the cross sections for inelastically scattering 14-Mev neutrons into 9- to 14-Mev energy range. The cross section for producing these high-energy neutrons, which may be attributed to direct interaction processes, is roughly 10% of the nonelastic cross section, for all elements. A comparison is made with data of Coon and co-workers, who measured angular distributions for the samc high-energy inelastically scattered neutron group. (auth)
Date: May 19, 1958
Creator: MacGregor, M. H.
Object Type: Report
System: The UNT Digital Library
Direct Interaction Neutrons from 14-Mev Inelastic Neutron Scattering (open access)

Direct Interaction Neutrons from 14-Mev Inelastic Neutron Scattering

Abstract: "Neutron nonelastic cross sections measured at different detector biases have been used to determine the cross sections for inelastically scattering 14 Mev neutrons into 9- to 14-Mev energy range. The cross section for producing these high energy neutrons, which may be attributed to direct interaction processes, is roughly 10% of the nonelastic cross section, for all elements. A comparison is made with data of Coon and co workers, who measured angular distributions for the same high-energy inelastically scattered-neutron group."
Date: May 19, 1958
Creator: MacGregor, Malcolm H.
Object Type: Report
System: The UNT Digital Library
Fused Lithium Salts: A Bibliography Covering 1950-57 (open access)

Fused Lithium Salts: A Bibliography Covering 1950-57

None
Date: May 19, 1958
Creator: Baughman, D. & Maynard, G.R.
Object Type: Report
System: The UNT Digital Library
Fused Lithium Salts : A Bibliography Covering 1950-57 (open access)

Fused Lithium Salts : A Bibliography Covering 1950-57

This is a bibliography referencing documents based on fused lithium salts within the years 1950-57.
Date: May 19, 1958
Creator: Baughman, Dorothy & Maynard, G. R.
Object Type: Report
System: The UNT Digital Library
Hanford Atomic Products Operation Five-Year Program (open access)

Hanford Atomic Products Operation Five-Year Program

The General Electric Company has prepared in past years numerous documents for the Atomic Energy Commission outlining in some detail its current and proposed programs at Hanford. Last year, at the request of the commission, program types of information were consolidated into one document, the HAPO Five Year Program. That document was well received and useful to an extent that the General Electric Company was requested by the Commission to prepare another covering the fiscal years 1959 through 1963. In outlining the five year program for the Hanford Atomic Products Operation, the General Electric Company has made assumptions regarding the US Atomic Energy Commission`s current and future programs and Hanford`s relationship to these programs. Two major objectives of the Commission were considered basic for future planning: first, to provide adequate atomic weapons for national defense; and second, to encourage and assist in the development of atomic energy for peaceful uses. The Hanford contributions to these objectives are conceived to include the acquisition and potential application of new technology in support of: (1) Increased production of plutonium, as nitrate solution, buttons, and as current and future shapes. (2) A program that will provide the technological capability to implement broad changes in …
Date: May 19, 1958
Creator: Priode, C. A.; Benoliel, R. W.; Gilbert, W. D.; McGrath, R. E.; Tomlinson, R. E. & Zuhr, H. F.
Object Type: Report
System: The UNT Digital Library
Neutron Nonelastic Cross-Section Measurements from 7 to 29 Mev (open access)

Neutron Nonelastic Cross-Section Measurements from 7 to 29 Mev

Abstract: "Neutron nonelastic cross sections have been measured for 23 elements at 14 Mev, and for a selected set of these elements over the energy ranges 7 to 14 Mev and 21 to 29 Mev. Conventional sphere transmission techniques were used for the measurements. A comparison with optical model calculations of Bjorklund and Fernbach shows excellent agreement."
Date: May 19, 1958
Creator: MacGregor, Malcolm H.
Object Type: Report
System: The UNT Digital Library
Performance of a 28-inch ramjet utilizing gaseous hydrogen at a Mach number of 3.6, angles of attack up to 12 degree, and pressure altitudes up to 110,000 feet (open access)

Performance of a 28-inch ramjet utilizing gaseous hydrogen at a Mach number of 3.6, angles of attack up to 12 degree, and pressure altitudes up to 110,000 feet

Report presenting an investigation in the 10- by 10-foot supersonic wind tunnel to evaluate the performance of a shrouded injector burner with perforated domes employed in a 28-inch ramjet using gaseous hydrogen as fuel. Steady-state data were obtained at a pressure altitude of 77,000 feet and zero angle of attack. Results indicated that burning could be initiated under severe distortion conditions and that satisfactory combustor operation was accomplished up to a pressure altitude of 110,000 feet with no adverse effect on combustion efficiency.
Date: May 19, 1958
Creator: Musial, Norman T.; Ward, James J. & Wasserbauer, Joseph F.
Object Type: Report
System: The UNT Digital Library