States

The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65 (open access)

The effect of blade-section thickness ratio on the aerodynamic characteristics of related full-scale propellers at Mach numbers up to 0.65

The results of an investigation of two 10-foot-diameter, two-blade NACA propellers are presented for a range of blade angles from 20 degrees to 55 degrees at airspeeds up to 500 miles per hour. These results are compared with those from previous investigations of five related NACA propellers in order to evaluate the effects of blade-section thickness ratios on propeller aerodynamic characteristics.
Date: April 25, 1949
Creator: Maynard, Julian D. & Steinberg, Seymour
Object Type: Report
System: The UNT Digital Library
General algebraic method applied to control analysis of complex engine types (open access)

General algebraic method applied to control analysis of complex engine types

"A general algebraic method of attack on the problem of controlling gas-turbine engines having any number of independent variables was utilized employing operational functions to describe the assumed linear characteristics for the engine, the control, and the other units in the system. Matrices were used to describe the various units of the system, to form a combined system showing all effects, and to form a single condensed matrix showing the principal effects. This method directly led to the conditions on the control system for noninteraction so that any setting disturbance would affect only its corresponding controlled variable" (p. 581).
Date: April 25, 1949
Creator: Boksenbom, Aaron S. & Hood, Richard
Object Type: Report
System: The UNT Digital Library
Investigations of an Annular Diffuser-Fan Combination Handling Rotating Flow (open access)

Investigations of an Annular Diffuser-Fan Combination Handling Rotating Flow

Memorandum presenting an investigation of two annular diffusers of different conical angles of expansion but constant outer diameters with rotating flow behind a fan. The performance characteristics are determined and the rotational-kinetic-energy effects on the overall energy transformation are observed over a range of inlet mach numbers from 0.1 to 0.44 and angles of flow up to 28 degrees.
Date: April 25, 1949
Creator: Schwartz, Ira R.
Object Type: Report
System: The UNT Digital Library
Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance (open access)

Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance

"Investigations were conducted in the Cleveland altitude wind tunnel to determine the performance and operational characteristics of the 19B-2, 19B-8, and 19XS-1 turbojet engines. One objective was to determine the effect of altitude, flight Mach number, and tail-pipe-nozzle area on the performance characteristics of the six-stage and ten-stage axial-flow compressors of the 19B-8 and 19XB-1 engines, respectively, The data were obtained over a range of simulated altitudes and flight Mach numbers" (p. 1).
Date: April 25, 1947
Creator: Dietz, Robert O. & Kuenzig, John K.
Object Type: Report
System: The UNT Digital Library
Determination of reactivity coefficients and rod calibration of D Pile. Interim report on Production Test No. 105-97-P (open access)

Determination of reactivity coefficients and rod calibration of D Pile. Interim report on Production Test No. 105-97-P

The test of March 7, 1947 was planned as a check on power coefficient values; however, an analysis of reactivity data gave evidence of a considerable flattening of ``A`` rod in the region between 0--75 inches out. A second test of longer duration was therefore made on April 1, 1947 in order to obtain a check calibration of this portion of the control rod. The results of this test verified the flattening of this portion of ``A`` rod. The redetermined power coefficients based on new rod calibrations are given.
Date: April 25, 1947
Creator: Kruesi, F. E.
Object Type: Report
System: The UNT Digital Library
Effects of Compressibility on the Characteristics of Five Airfoils (open access)

Effects of Compressibility on the Characteristics of Five Airfoils

Report presenting the results of pressure-distribution tests to determine the effects of compressibility on the characteristics of the NACA 66,2-215, 66,2-015, 65(216)-418, 16-212, and 23015 airfoil sections. Schileren photographs of the air flow and data on the wake characteristics was also obtained.
Date: April 25, 1947
Creator: Daley, Bernard N.
Object Type: Report
System: The UNT Digital Library
Flight Observations of Aileron Flutter at High Mach Numbers as Affected by Several Modifications (open access)

Flight Observations of Aileron Flutter at High Mach Numbers as Affected by Several Modifications

Report presenting an investigation of aileron flutter associated with high-speed flight. When the aileron control system was modified by installing a hydraulic irreversible unit, it was possible to delay aileron flutter and reduce its amplitude. Results regarding the aileron flutter with and without the modifications, analysis of the time histories for the control systems, and relation between aileron upfloat and flutter are provided.
Date: April 25, 1947
Creator: Spreiter, John R.; Galster, George M. & Cooper, George E.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-162 (open access)

Texas Attorney General Opinion: V-162

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: Exemption of insecticide which has been registered with the Commissioner of Agriculture, as agricultural insecticide, from registration with the State Health Officer as livestock insecticide.
Date: April 25, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-163 (open access)

Texas Attorney General Opinion: V-163

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: The designation of notes receivable as "property" within the meaning of Article XII, Section 6, Constitution of Texas.
Date: April 25, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-165 (open access)

Texas Attorney General Opinion: V-165

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: The applicability of the Securities Act to a group retirement plan issued by a non-profit group.
Date: April 25, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: O-7132 (open access)

Texas Attorney General Opinion: O-7132

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: Authority of State Library to purchase microfilm copies of certain newspapers, and to microfilm newspapers in lieu of "binding" same as provided by Article 5441, R.C.S.
Date: April 25, 1946
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed (open access)

Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed

Report presenting flight measurements of the pressures on the horizontal tail surfaces of a typical propeller-driven pursuit airplane during stalled pull-outs at high Mach number. Unit loads measured on the stabilizer at safe maneuvering limits were not only considerably in excess of the design unit loads, but also occurred in a direction opposite to the design loads. Revision of the tail-load design requirements and manner of specifying safe maneuverability limits to pilots appears necessary.
Date: April 25, 1944
Creator: Clousing, Lawrence A. & Turner, William N.
Object Type: Report
System: The UNT Digital Library
Photographic film as a pocket radiation dosimeter (open access)

Photographic film as a pocket radiation dosimeter

The energy dependence of film blackening is discussed and shown graphically. The exposure range of films is discussed, and blackening is plotted vs exposure for DuPont No. 502, and for the less sensitive DuPont No. 351. A plan is then described for monitoring radiation exposure to workers by requiring the worker to carry an x-ray film of dental packet size in a badge designed for the purpose. (LEW)
Date: April 25, 1944
Creator: Pardue, L. A.; Goldstein, N. & Wollan, E. O.
Object Type: Report
System: The UNT Digital Library
Watermanship (open access)

Watermanship

"The purpose of this manual is three-fold: a. To give you those basic principles of watermanship that will enable you to meet with confidence any emergency that may arise. b. To teach you certain fundamental practices used during small landing-craft operations. c. To show you how to swim small lakes or rivers under combat conditions."
Date: April 25, 1944
Creator: United States. War Department.
Object Type: Book
System: The UNT Digital Library
Texas Attorney General Opinion: O-3485 (open access)

Texas Attorney General Opinion: O-3485

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;Concerning rates to be charged by contract carriers and records to be kept by them.
Date: April 25, 1941
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Theory of ballooning. (open access)

Theory of ballooning.

A general guide to piloting a free balloon.
Date: April 25, 1940
Creator: United States. War Department.
Object Type: Book
System: The UNT Digital Library