Preliminary Report on Thermal and Electrical Conductivities of Some Plutonium-Aluminum Alloys (open access)

Preliminary Report on Thermal and Electrical Conductivities of Some Plutonium-Aluminum Alloys

Abstract: "The thermal and electrical conductivities of a series of Pu-Al alloys have been determined in the range 0.12 atomic percent Pu. The conductivities are approximately proportional to the volume of free aluminum."
Date: March 15, 1950
Creator: Gibney, Robert B. & Sandenaw, Thomas A.
System: The UNT Digital Library
TTA Analysis (open access)

TTA Analysis

Paper describes procedures used at Hanford to bioassay plutonium in urine samples.
Date: March 15, 1950
Creator: Healy, J. W.
System: The UNT Digital Library
NUCLEAR PHYSICS RESEARCH AT COLUMBIA UNIVERSITY (open access)

NUCLEAR PHYSICS RESEARCH AT COLUMBIA UNIVERSITY

None
Date: March 15, 1950
Creator: Dunning, J.R. Director
System: The UNT Digital Library
High-Speed Aerodynamic Characteristics of a Lateral-Control Model 2: Modified NACA 0012-64 Section with a 26.6-Percent-Chord, Plain, Trailing-Edge Aileron; Wing Unswept and Swept Back 45 Degrees (open access)

High-Speed Aerodynamic Characteristics of a Lateral-Control Model 2: Modified NACA 0012-64 Section with a 26.6-Percent-Chord, Plain, Trailing-Edge Aileron; Wing Unswept and Swept Back 45 Degrees

Memorandum presenting wind tunnel tests to determine the aerodynamic characteristics of a semispan wing with a modified NACA 0012-64 section and a 26.6-percent-chord, plain, trailing-edge aileron. Results are shown for the wing with the 0.229-chord line unswept and swept back 45 degrees and for a Mach number range from 0.40 to 0.925.
Date: March 15, 1950
Creator: Krumm, Walter J. & Anderson, Joseph L.
System: The UNT Digital Library
Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line (open access)

Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line

"The method of superposition of linearized conical flows has been applied to the calculation of the aerodynamic properties, in supersonic flight, of thin flat, swept-back wings at an angle of attack. The wings are assumed to have rectilinear plan forms, with tips parallel to the stream, and to taper in the conventional sense. The investigation covers the moderately supersonic speed range where the Mach lines from the leading-edge apex lie ahead of the wing" (p. 1147).
Date: March 15, 1950
Creator: Cohen, Doris
System: The UNT Digital Library
Protactinium Chemistry (open access)

Protactinium Chemistry

Report discussing protactinium, including the element's history and the results of various experiments.
Date: March 15, 1950
Creator: Elson, R. E.; Sullivan, J. C.; Studier, N. H. & Sullens, P. A.
System: The UNT Digital Library