The Effect of the Maxwell Distribution of Velocities on the Neutron Density and Diffusion Length in a Metal Sphere (open access)

The Effect of the Maxwell Distribution of Velocities on the Neutron Density and Diffusion Length in a Metal Sphere

The change in the simple [formula] distribution of neutrons in a spherical lump of uranium caused by the distribution in velocities of thermal neutrons is calculated. If the calculated curve is fitted as well as possible by a simple [formula] curve, it is shown that the value of [formula] obtained in this way is a function of [formula], the radius of the sphere. For small radii the [formula] obtained in this manner will be as much as 25% greater than the [formula] corresponding to average velocity neutrons. The change in the thermal utilization caused by the distribution in velocities is discussed. The flux of neutrons into a sphere is calculated taking into account the velocity distribution and this is compared with the usual theory.
Date: June 27, 1944
Creator: Plass, Gilbert N.
Object Type: Report
System: The UNT Digital Library
Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4 (open access)

Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4

An investigation of the damping-in-roll characteristics of three wings with an aspect ratio of 4, a taper ratio of 0.6, three sweep angles at the quarter chord line, and the NACA 65A006 section as determined through a range of Mach numbers and angles of attack.
Date: June 27, 1949
Creator: Kuhn, Richard E. & Myers, Boyd C., II
Object Type: Report
System: The UNT Digital Library
Stick-Fixed Stability and Control Characteristics of the Consolidated Vultee Model 240 Airplane as Estimated from Tests of a 0.092-Scale Powered Model (open access)

Stick-Fixed Stability and Control Characteristics of the Consolidated Vultee Model 240 Airplane as Estimated from Tests of a 0.092-Scale Powered Model

From Summary: "Estimates of the static stick-fixed stability and control characteristics of the Consolidated Vultee model 240 airplane are presented in this report. The estimates are based on tests of a 0.092-scale powered model in the 10-foot wind tunnel of the Guggenheim Aeronautical Laboratory of the California Institute of Technology. Results of the analysis are evaluated in terms of the Army specifications for stability and control characteristics which are more specific and, in general, equal to or more rigid than the Civil Aeronautics Administration requirements."
Date: June 27, 1947
Creator: McCullough, George B.; Weiberg, James A. & Gault, Donald E.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: O-2013A (open access)

Texas Attorney General Opinion: O-2013A

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, Gerald Mann, regarding a legal question submitted for clarification: Authority of McLennan County to participate in the U.S. Government plan of surplus commodities distribution.
Date: June 27, 1940
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: O-6002 (open access)

Texas Attorney General Opinion: O-6002

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, Grover Sellers, regarding a legal question submitted for clarification: Does County Commissioner of Swisher County have to file itemized verified account each month in order to be allowed traveling expenses under Art. 2350(7), V. C. S.
Date: June 27, 1944
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Wind-Tunnel Investigation of a 1/5-Scale Model of the Ryan XF2R Airplane (open access)

Wind-Tunnel Investigation of a 1/5-Scale Model of the Ryan XF2R Airplane

"Wind-tunnel tests on a 1/5-scale model of the Ryan XF2R airplane were conducted to determine the aerodynamic characteristics of the air intake for the front power plant, a General Electric TG-100 gas turbine, and to determine the stability and control characteristics of the airplane. The results indicated low-dynamic-pressure recovery for the air intake to the TG-100 gas turbine with the standard propeller in operation. Propeller cuffs were designed and tested for the purpose of improving the dynamic-pressure recovery" (p. 1).
Date: June 27, 1947
Creator: Wong, Park Y.
Object Type: Report
System: The UNT Digital Library