'Fission' of Medium Weight Elements (open access)

'Fission' of Medium Weight Elements

The fission reaction has been observed with high energy accelerator projectiles for elements as light as tantalum but has not been reported for medium weight elements. The present note presents evidence for the occurrence of reactions which are probably most properly described by the term 'fission' and which seem to occur with very small yield throughout the region where this type of reaction is only slightly exoergic or even endoergic with respect to mass balance. In the course of detailed investigation of the spallation of copper and the variation of the product yields with energy of the bombarding particle the threshold for formation of radioactive Cl{sup 38} (38-minute half-life) from elemental studied. The energetically most economical way in which Cl{sup 38} might be spallation reactions is by emission from the bombarded copper nucleus of nucleons in groups such as alpha-particles instead of single nucleons 0 The energetic requirements for the reaction Cu{sup 63}(p,pn6a)Cl{sup 38}, in which the maximum number of alpha-particles are emitted, include (1) the mass difference between the reactants and the products and (2) the excitation energy which the alpha-particles must have in order to pass over the coulombic barrier, Since the reaction is endoergic with respect to …
Date: May 29, 1950
Creator: Batzel, Roger T. & Seaborg, G. T.
Object Type: Report
System: The UNT Digital Library
Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311 (open access)

Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311

"An investigation has been conducted in the Langley 20-foot free-spinning tunnel to determine the spin and recovery characteristics of a 0.057-scale model of the modified Chance Vought XF7U-1 airplane. The primary change in the design from that previously tested was a revision of the twin vertical tails. Tests were also made to determine the effect of installation of external wing tanks" (p. 1).
Date: May 29, 1950
Creator: Berman, Theodore & Pumphrey, Norman E.
Object Type: Report
System: The UNT Digital Library
On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid (open access)

On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid

"The particular integrals of the second-order and third-order Prandtl-Busemann iteration equations for the flow of a compressible fluid are obtained by means of the method in which the complex conjugate variables are utilized as the independent variables of the analysis. The assumption is made that the Prandtl-Glauert solution of the linearized or first-order iteration equation for the two-dimensional flow of a compressible fluid is known. The forms of the particular integrals, derived for subsonic flow, are readily adapted to supersonic flows with only a change in sign of one of the parameters of the problem" (p. 909).
Date: May 29, 1950
Creator: Kaplan, Carl
Object Type: Report
System: The UNT Digital Library
Recovery of Nitric Acid in the Tributyl Phosphate Process for Uranium Recovery. Part 2. (open access)

Recovery of Nitric Acid in the Tributyl Phosphate Process for Uranium Recovery. Part 2.

Report discussing study on recovery of nitric acid in the uranium recovery process. The behavior of chloride ions and tributyl phophate is noted, and the quality of recycled nitric acid was tested. Stainless steel in the nitric acid recovery system was evaluated for corrosion.
Date: May 29, 1950
Creator: Wagner, R. M. & Groot, C.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-1064 (open access)

Texas Attorney General Opinion: V-1064

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, Price Daniel, regarding a legal question submitted for clarification: Taxation of a whip owned by a Louisiana corporation and listing Corpus Christi, Texas, as its home port.
Date: May 29, 1950
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Corrosion Newsletter No. 3 (open access)

Corrosion Newsletter No. 3

None
Date: May 29, 1951
Creator: English, J. L.
Object Type: Journal/Magazine/Newsletter
System: The UNT Digital Library
Division of Load Among the Wing, Fuselage, and Tail of Aircraft (open access)

Division of Load Among the Wing, Fuselage, and Tail of Aircraft

Report discussing the division of load among the wing, fuselage, and tail for several aircraft configurations at subsonic and supersonic speeds. The load that each component carries at various Mach numbers and angles of attack is described.
Date: May 29, 1951
Creator: Mayer, John P. & Gillis, Clarence L.
Object Type: Report
System: The UNT Digital Library
On the Development of Turbulent Wakes From Vortex Streets (open access)

On the Development of Turbulent Wakes From Vortex Streets

"Wake development behind circular cylinders at Reynolds numbers from 40 to 10,000 was investigated in a low-speed wind tunnel. Standard hot-wire techniques were used to study the velocity fluctuations. The Reynolds number range of periodic vortex shedding is divided into two distinct subranges" (p. 1).
Date: May 29, 1952
Creator: Roshko, Anatol
Object Type: Report
System: The UNT Digital Library
Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap (open access)

Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap

From Introduction: "The present report gives results at a Mach number of 4.04 of the part of the program concerned with flap controls at Mach numbers from 1.62 to 6.9."
Date: May 29, 1953
Creator: Dunning, Robert W. & Ulmann, Edward F.
Object Type: Report
System: The UNT Digital Library
Altitude investigation of XJ34-WE-32 engine performance without electronic control (open access)

Altitude investigation of XJ34-WE-32 engine performance without electronic control

From Introduction: "As a part of the comprehensive investigation of the XJ34-WE-32 engine conducted in the NACA Lewis altitude wind tunnel, the over-all-performance was determined over a range of altitudes and flight Mach numbers. Other phases of the investigation are reported in reference 1. The results are given in tables and also in graphical form to show the trends of engine performance associated with changes of altitude, flight Mach number, and exhaust-nozzle area."
Date: May 29, 1953
Creator: Bloomer, Harry E.; Walker, William J. & Pantages, George L.
Object Type: Report
System: The UNT Digital Library
Altitude Performance Investigation of Two Single-Annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor With Various Combustor-Inlet Air Pressure Profiles (open access)

Altitude Performance Investigation of Two Single-Annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor With Various Combustor-Inlet Air Pressure Profiles

Report presenting data obtained three single annular-type combustors with different combustor inlet-air pressure profiles over a range of engine speeds. Results regarding effect of changing combustor inlet-air pressure profile and hole geometry on combustor performance, performance of the prototype J40-WE-8 turbojet engine combustor, correlation of combustion efficiency with engine fuel-air ratio and combustion parameter, and comparison of several combustors from different turbojet engines are provided.
Date: May 29, 1953
Creator: Sobolewski, Adam E.; Miller, Robert R. & McAulay, John E.
Object Type: Report
System: The UNT Digital Library
Effects of High Degrees of Biaxial Stretch Forming on Crazing and Other Properties of Acrylic Plastic Glazing (open access)

Effects of High Degrees of Biaxial Stretch Forming on Crazing and Other Properties of Acrylic Plastic Glazing

Memorandum presenting an investigation of the effects of higher degrees of forming in biaxial stretch-forming of polymethyl methacrylate to about 50-percent strain. Sheets of commercial cast polymethyl methacrylate were hot-stretched approximately 100 and 150 percent, respectively, and tests were conducted on this material and on unstretched cotton material. Results regarding the standard tensile tests, stress-solvent crazing, surface abrasion tests, and x-ray diffraction patterns are provided.
Date: May 29, 1953
Creator: Wolock, I.; Axilrod, B. M. & Sherman, M. A.
Object Type: Report
System: The UNT Digital Library
Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio (open access)

Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio

Report presenting an investigation to determine the effects of plan-form taper on the aerodynamic characteristics of a series of symmetrical, unswept wings with thicknesses of 8-percent chord. The wings were tested with four different bodies of revolution over a range of Mach numbers. Results regarding the lift, drag, pitching-moment, lift-curve slope, lift-drag ratio, and pitching-moment curve are provided.
Date: May 29, 1953
Creator: Allen, Edwin C.
Object Type: Report
System: The UNT Digital Library
Preliminary investigation of the effect of fences and balancing tabs on the hinge-moment characteristics of a tip control on a 60 degree delta wing at Mach number 1.61 (open access)

Preliminary investigation of the effect of fences and balancing tabs on the hinge-moment characteristics of a tip control on a 60 degree delta wing at Mach number 1.61

Report presenting an investigation at Mach number 1.61 of the effects of chordwise fences and attached tabs on the hinge-moment characteristics of a half-delta tip control mounted on a 60 degree delta wing. Testing occurred over a range of angles of attack and control deflection. Results indicated that, in general, the effect of fences was to improve the linearity of hinge-moment curves and increase the negative values of slope parameters of hinge moment against control deflection and angle of attack.
Date: May 29, 1953
Creator: Czarnecki, K. R. & Lord, Douglas R.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-47 (open access)

Texas Attorney General Opinion: S-47

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: Application of Article 1111d, V.P.C., as amended, the chain store tax, upon concession stands within carnivals.
Date: May 29, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-48 (open access)

Texas Attorney General Opinion: S-48

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: Application of occupation tax levied by virtue of Section 7 of Article 7047, V.C.S., upon livestock clearing houses and those persons utilizing the clearing house services.
Date: May 29, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Wind-Tunnel Investigation at High Subsonic Speeds of a Spoiler-Slot Deflector Combination on an NACA 65A006 Wing With Quarter-Chord Line Swept Back 32.6 Degrees (open access)

Wind-Tunnel Investigation at High Subsonic Speeds of a Spoiler-Slot Deflector Combination on an NACA 65A006 Wing With Quarter-Chord Line Swept Back 32.6 Degrees

Report presenting an investigation in the high-speed tunnel for a range of Mach numbers to determine the lateral control characteristics of a wing-fuselage combination with the wing quarter-chord line swept back 32.6 degrees, an aspect ratio of 4, a taper ratio of 0.6, and an NACA 65A006 section. Results regarding yawing-moment characteristics, spoiler-slot-deflector testing, and rolling-moment coefficient are provided.
Date: May 29, 1953
Creator: Vogler, Raymond D.
Object Type: Report
System: The UNT Digital Library
Preliminary Draft - Economics of Waste Disposal (open access)

Preliminary Draft - Economics of Waste Disposal

None
Date: May 29, 1956
Creator: Culler, Jr., Floyd L.
Object Type: Report
System: The UNT Digital Library
Production test number 105-634-A in-pile cocked slug tests (open access)

Production test number 105-634-A in-pile cocked slug tests

Slug ruptures characterized by intergranular corrosion failure of the aluminum can (Hot Spot Ruptures) have been a major cause for loss of reactor production, particularly during the past year. Although the cause for these failures is not definitely known, it is suspected that fuel elements when cocked in the process tube will sufficiently distort the neutron flux and the heat transfer characteristics in a localized area that very high local temperatures will exist and the corrosion rate of the aluminum can in these areas will be accelerated. It is the purpose of this test to introduce slugs that are known to be cocked and compare their resistance to rupture with slugs that are known to be uncocked when initially charged.
Date: May 29, 1956
Creator: McCarthy, P. B. & VanWormer, F. W.
Object Type: Report
System: The UNT Digital Library
Reactor Analysis for the Army Package Power Reactor No. 1 (open access)

Reactor Analysis for the Army Package Power Reactor No. 1

Abstract: The reactor analysis of the critical experiment and the APPR-1 resulted in a loading of the APPR-1 of 31.096 gm of B-10 with 22.5 kg U-335. This loading will result in adequate reactivity for a core life of 13 MWYR based on uniform burnup of U-335 and B-10. Calculations indicate that five of the seven control rods provided are more than adequate to shut the reactor down at any time. The temperature coefficient of reactivity should be at least -2 x 10-4 [delta] K/0F.
Date: May 29, 1956
Creator: Gallagher, J. G.; Giesler, H. W.; Johnson, W. R.; Fairbanks, F. B.; Oby, P. V. & Crouch, A. N.
Object Type: Report
System: The UNT Digital Library
Reactor Analysis for the Army Package Power Reactor No. 1 (open access)

Reactor Analysis for the Army Package Power Reactor No. 1

Abstract: The reactor analysis of the critical experiment and the APPR-1 resulted in a loading of the APPR-1 of 31.096 gm of B-10 with 22.5 kg U-335. This loading will result in adequate reactivity for a core life of 13 MWYR based on uniform burnup of U-335 and B-10. Calculations indicate that five of the seven control rods provided are more than adequate to shut the reactor down at any time. The temperature coefficient of reactivity should be at least -2 x 10-4 [delta] K/0F.
Date: May 29, 1956
Creator: Gallagher, J. G.; Giesler, H. W.; Johnson, W. R.; Fairbanks, F. B.; Oby, P. V. & Crouch, A. N.
Object Type: Report
System: The UNT Digital Library
SEMI-ANNUAL SUMMARY RESEARCH REPORT IN METALLURGY FOR JULY-DECEMBER, 1955 (open access)

SEMI-ANNUAL SUMMARY RESEARCH REPORT IN METALLURGY FOR JULY-DECEMBER, 1955

None
Date: May 29, 1956
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: S-199 (open access)

Texas Attorney General Opinion: S-199

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: Proper method for fixing franchise tax liability of a corporation dissolving within one year after incorporation.
Date: May 29, 1956
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History