Effects of Combinations of Aspect Ratio and Sweepback at High Subsonic Mach Numbers (open access)

Effects of Combinations of Aspect Ratio and Sweepback at High Subsonic Mach Numbers

Report discussing an investigation to determine the effects of sweepback and low aspect ratio on the aerodynamic characteristics of a wing at high subsonic Mach numbers. Tests were performed at aspect ratios of 2, 3, and 5 and sweepback angles of 0, 30, and 45 degrees. Generally, sweepback and low aspect ratio were found to both delay and lessen the effects of compressibility.
Date: June 4, 1947
Creator: Adler, Alfred A.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-233 (open access)

Texas Attorney General Opinion: V-233

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: Authority of Prison Board to direct general manager to permit the use of inmate labor on sewer project with City of Huntsville.
Date: June 4, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-237 (open access)

Texas Attorney General Opinion: V-237

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: Constitutionality of H.B. 309 amending Article 480a, Penal Code 1925.
Date: June 4, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream (open access)

Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream

From Summary: "A theoretical study, based on the linearized equations of motion for small disturbance, is made of the air forces on wings of general plan forms moving forward at a constant supersonic speed. The boundary problem is set up for both the harmonically oscillating and the steady conditions. Two types of boundary conditions are distinguished, which are designated "purely supersonic" and "mixed supersonic." the method is illustrated by applications to a number of examples for both the steady and the oscillating conditions."
Date: June 4, 1947
Creator: Garrick, I. E. & Rubinow, S. I.
Object Type: Report
System: The UNT Digital Library