Determination of Organic Acids in Process Solutions (open access)

Determination of Organic Acids in Process Solutions

Abstract: "A method has been established for the estimation of volatile organic acids in aqueous process solutions containing UNH, nitric acid, ANN, sodium dichromate and small amounts of hexone. The practice is to distill a 400 ul or 500 ul sample in the presence of an excess of phosphoric acid and ferrous sulfate under a high vacuum; a special apparatus utilizing a receiver cooled with a dry ice-isopropanol mixture is employed. The distillate is taken up in isopropanol and then titrated potentiometrically with standard potassium hydroxide solution. Since nitric acid and organic acids are present, two end points are observed. The potassium hydroxide added between these end points is equivalent to the organic acids. In the titration, CO2 from the atmosphere or in the potassium hydroxide is a source of error. The former was avoided and correction was made for the latter."
Date: June 29, 1949
Creator: Brouns, R. J. & Pollock, C. W.
System: The UNT Digital Library
Initial Flight Test of the NACA FR-1-A, a Low-Acceleration Rocket-Propelled Vehicle for Transonic Flutter Research (open access)

Initial Flight Test of the NACA FR-1-A, a Low-Acceleration Rocket-Propelled Vehicle for Transonic Flutter Research

Report presenting testing on the first of a series of flutter rockets, designated the NACA FR-1-A, which was tested with two identical swept wings. Results regarding the launching, flight, and wing failure are provided.
Date: June 29, 1948
Creator: Angle, Ellwyn E.
System: The UNT Digital Library
The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model (open access)

The Effects of Fuel Sloshing on the Lateral Stability of a Free-Flying Airplane Model

Memorandum presenting an investigation in the free-flight tunnel to determine the effect of the sloshing of fuel in partly filled, unbaffled tanks on the lateral stability of a free-flying model. Flight tests were made to determine the effects of the water sloshing for different depths of water and various masses and moments of inertia of the model. The sloshing caused small-amplitude, high-frequency lateral oscillations which were superimposed on the normal Dutch roll oscillation so that the lateral motions of the model appeared jerky.
Date: June 29, 1948
Creator: Smith, Charles C., Jr.
System: The UNT Digital Library
Experimental determination of the subsonic performance of a ram-jet unit containing thin-plate burners (open access)

Experimental determination of the subsonic performance of a ram-jet unit containing thin-plate burners

Report presenting the performance of a ramjet unit consisting of an intake diffuser, an exhaust nozzle, and a cluster of thin-plate burners contained in a semicircular combustion chamber as investigated in the induction aerodynamics laboratory.
Date: June 29, 1949
Creator: Henry, John R.
System: The UNT Digital Library
Events of importance for week ending June 29, 1949, Hanford Operations Office, Richland, Washington (open access)

Events of importance for week ending June 29, 1949, Hanford Operations Office, Richland, Washington

This report details events of importance as reported by the Hanford Operations Office for the week ending June 29, 1949.
Date: June 29, 1949
Creator: Schlemmer, F. C.
System: The UNT Digital Library
Stability of Split Hollow Cylinders (open access)

Stability of Split Hollow Cylinders

Abstract: "The behavior of radially split hollow cylinders upon heating is discussed."
Date: June 29, 1944
Creator: Karush, William & Monk, A. T.
System: The UNT Digital Library
Atomic Displacements Produced by Fission Fragments and Fission Neutrons in Matter (open access)

Atomic Displacements Produced by Fission Fragments and Fission Neutrons in Matter

About four-fifths of the energy of the fission process is shared by the two heavy fragments into which the nucleus splits. This energy, of about 80 Mev. per fragment, is transferred to the medium in which the fission takes place in two ways. First, because each fragment is stripped of about half of its electrons during most of its path, it will interact strongly with electrons and thus lose energy through ionizing collisions with other atoms. Secondly, the fragments will lose energy by elastic collisions with atoms as a whole. Each fragment leaves in its wake a cloud of moving electrons and atoms. This cloud will roughly resemble a cylinder whose radius will increase with time on account of the motion of the struck electrons and atoms. They may now investigate two features of the slowing down process. First as it affects the fragment, i.e. we calculate its range, straggling, etc. And secondly they may work out the motion of the cylinder of moving particles, its effect on the medium, etc.
Date: June 29, 1949
Creator: Ozeroff, J.
System: The UNT Digital Library