Texas Attorney General Opinion: S-37 (open access)

Texas Attorney General Opinion: S-37

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: Constitutionality of House Bill 93, Acts 51st Legislature, Regular Session, 1949, chapter 368, page 702 and House Bill 196, Acts 52nd Legislature, Regular Session, 1951, chapter 156, page 270, relative to the establishment of juvenile courts.
Date: May 5, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow (open access)

Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow

Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect ratios and taper ratios and with a variety of angle-of-attack or twist distributions, including flap and aileron deflections, by means of the Weissinger method with eight control points on the semispan. Also calculated were aerodynamic influence coefficients which pertain to a certain definite set of stations along the span, and several methods are presented for calculating aerodynamic influence functions and coefficients for stations other than those stipulated. The information presented in this report can be used in the analysis of untwisted wings or wings with known twist distributions, as well as in aeroelastic calculations involving initially unknown twist distributions.
Date: May 5, 1953
Creator: Diederich, Franklin W. & Zlotnick, Martin
Object Type: Report
System: The UNT Digital Library
Comparison of the aerodynamic characteristics at transonic speeds of a plane wing and a cambered and twisted wing, both having 45 degrees of sweepback and an aspect ratio of 6 (open access)

Comparison of the aerodynamic characteristics at transonic speeds of a plane wing and a cambered and twisted wing, both having 45 degrees of sweepback and an aspect ratio of 6

Report presenting a transonic investigation made by the free-fall technique of a plane wing and a cambered and twisted wing, each with an aspect ratio 6, taper ratio of 0.5, and a sweepback of 45 degrees. Measurements were made of the loads on the exposed wings, pressures on the fuselage in the vicinity of the wing, and acceleration and angle of attack of the complete model.
Date: May 5, 1953
Creator: Holdaway, George H.
Object Type: Report
System: The UNT Digital Library
Process modifications 202-S building (open access)

Process modifications 202-S building

A scheme was proposed whereby the third and second uranium cycle salt wastes in the Redox plant are combined, stripped, evaporated, and then returned as scrub to the first (and possibly second) cycles as scrub, operating as a dual scrub column. It is the purpose of this report to study this proposed method of back-cycling, and to investigate other methods of reducing chemical and waste storage costs.
Date: May 5, 1953
Creator: Rohrmann, C. A. & Ludloy, J. O.
Object Type: Report
System: The UNT Digital Library