Texas Attorney General Opinion: V-36 (open access)

Texas Attorney General Opinion: V-36

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: Liability for the one (1) per cent Motor Vehicle Retail Sales Tax levied by Art. 7047k, V.A.C.S., where motor vehicles owned by a partnership are transferred to the corporation.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-37 (open access)

Texas Attorney General Opinion: V-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, Price Daniel, regarding a legal question submitted for clarification: Fees due a Constable for transporting a prisoner from the county in which detained to the county in which charged, and related matters.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-39 (open access)

Texas Attorney General Opinion: V-39

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: Whether or not the proviso to Art. 7298, Rev. Stat., Vernon's Codification, is a statue of limitation which must be pleaded by the taxpayer.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-40 (open access)

Texas Attorney General Opinion: V-40

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 the Commissioners' Court of Throckmorton County to sell personal property such as worn out road machinery without first having advertised the same for sale on open bids; and authority of the Tax Collector to make summary levy on personal property as provided in Article 7268.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-41 (open access)

Texas Attorney General Opinion: V-41

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: Proper officer for collecting the delinquent taxes which have accrued before a Water Control and Improvement District, pursuant to the provisions of Article 1066b, authorizes the Tax Collector of the municipality within which it is wholly located to act in its behalf as Tax Collector.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-43 (open access)

Texas Attorney General Opinion: V-43

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: Application for reimbursement for special education, signature of County Superintendent, necessity for under Article 2922-3, Section 2, V.A.C.S.
Date: February 21, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines (open access)

Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines

"On the basis of a recently developed theory for finite sweptback wings at supersonic speeds, calculations of the supersonic wave drag at zero lift were made for a series of wings having thin symmetrical biconvex sections with untapered plan forms and various angles of sweepback and aspect ratios. The results are presented in a unified form so that a single chart permits the direct determination of the wave drag for this family of airfoils for an extensive range of aspect ratio and sweepback angle for stream Mach numbers up to a value corresponding to that at which the Mach line coincides with the wing leading edge. The calculations showed that in general the wave-drag coefficient decreased with increasing sweepback" (p. 1).
Date: February 21, 1947
Creator: Harmon, Sidney M. & Swanson, Margaret D.
Object Type: Report
System: The UNT Digital Library
Preliminary Tests at Supersonic Speeds of Triangular and Swept-Back Wings (open access)

Preliminary Tests at Supersonic Speeds of Triangular and Swept-Back Wings

Report presenting testing of a series of thin, triangular plan-form wings, including eight triangular wings of vertex angles and three swept-back wings with circular-arc sections. Results regarding lift, center of pressure, and ideal operation of different types of wings are provided.
Date: February 21, 1947
Creator: Ellis, Macon C., Jr. & Hasel, Lowell E.
Object Type: Report
System: The UNT Digital Library
Investigation of High-Performance Fuels in Multicylinder and in Single-Cylinder Engines at High and Cruising Engine Speeds (open access)

Investigation of High-Performance Fuels in Multicylinder and in Single-Cylinder Engines at High and Cruising Engine Speeds

"An investigation was conducted to compare the knock-limited performance of a 20-percent triptane blend in 28-K fuel with that of 28-R and 33-R fuels at high engine speeds, cruising speeds, and two compression ratios in an K-1830-94 multicylinder engine. Data were obtained with the standard compression ratio of 6.7 and with a compression ratio of 3.0. The three fuels were investigated at engine speeds of 1800, 2250, 2600, and 2800 rpm at high and low blower ratios" (p. 1).
Date: February 21, 1947
Creator: Bell, Arthur H.; Nelson, R. Lee & Richard, Paul H.
Object Type: Report
System: The UNT Digital Library