Resource Type

States

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings (open access)

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings

Report presenting an investigation of an 18-foot-radius helicopter rotor powered by tip-mounted ramjet engines in the helicopter test tower. The engine performance is compared with the performance determined in a previous investigation of a 9-foot-radius rotor with the same engines at similar speeds but with twice the centrifugal forces. Results regarding the propulsive characteristics, minimum specific fuel consumption and corresponding propulsive thrust, and operational characteristics are provided.
Date: October 7, 1953
Creator: Radin, Edward J. & Carpenter, Paul J.
Object Type: Report
System: The UNT Digital Library
A Rapid Method for Determining Preferred Orientation in Rolled Uranium Rods (open access)

A Rapid Method for Determining Preferred Orientation in Rolled Uranium Rods

Report covering an experiment on a method for determining the crystallographic orientation within uranium rods. From summary: "The crystallographic orientation existing in rolled uranium rods may be determined by comparing the diffraction pattern obtained from an unknown specimen with the diffraction pattern obtained from a sample known to be randomly oriented."
Date: January 7, 1953
Creator: Sanderson, M. J.; Cummings, W. V., Jr. & Hurst, R. P.
Object Type: Report
System: The UNT Digital Library
Proposed construction of Priest Rapids Dam in relation to Hanford Works (open access)

Proposed construction of Priest Rapids Dam in relation to Hanford Works

This paper summarizes the proposed construction of the Priest Rapids Dam on the Columbia River by the Atomic Energy Commission. Power generation to the Hanford Works and flood control for the surrounding area is the main goal for the construction of the dam. The summary covers the feasibility of the dam from its design, operation, benefits, security, drawbacks, etc.
Date: January 7, 1953
Creator: Smothers, S. A.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: MS-15 (open access)

Texas Attorney General Opinion: MS-15

Letter opinion 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; Legality of "waiver-teachers" voluntarily discontinuing membership in the retirement system after having once established such membership.
Date: April 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-16 (open access)

Texas Attorney General Opinion: MS-16

Letter opinion 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.
Date: April 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-17 (open access)

Texas Attorney General Opinion: MS-17

Letter opinion 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; Several questions relating to the authority of the commissioners' court respecting petitions calling for creation of navigation districts.
Date: April 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-72 (open access)

Texas Attorney General Opinion: MS-72

Letter opinion 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; Applicability of the penalty interest rate on delinquent school land purchase contracts during the grace period following the purchaser's death in which forfeiture of the land is forbidden under Article 5326, V.C.S.
Date: July 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: MS-99 (open access)

Texas Attorney General Opinion: MS-99

Letter opinion 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; Payment for services of Distributing Agents of Commodity Distribution Division of Department of Public Welfare, and for shipping and/or delivery charges on commodities recieved from the Federal Government.
Date: October 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-24 (open access)

Texas Attorney General Opinion: S-24

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: Applicability of the registration requirements of the Texas Livestock Remedy Act to manufacturers who sell only to veterinarians.
Date: April 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-25 (open access)

Texas Attorney General Opinion: S-25

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: Legality of paying the Criminal District Attorney of Gregg County $500.00 per year from State funds in accordance with Section 21 of Article V, Constitution of Texas.
Date: April 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-38 (open access)

Texas Attorney General Opinion: S-38

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: Highway Department's interest in illegally collected, non-resident, registration fees and its authority to collect same from the county.
Date: May 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: S-82 (open access)

Texas Attorney General Opinion: S-82

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: Mandatory or permissive character of the tax assessor-collector's function to issue tax certification.
Date: August 7, 1953
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Chemical Development, Quarterly Progress Report, July-September, 1953. (open access)

Chemical Development, Quarterly Progress Report, July-September, 1953.

Introduction: "During the last quarter, members of the Chemical Development Group have been concerned with six major projects. (1) thermal and radiation properties of organic materials as moderators and coolants, (2) thermal and radiation stability of mirconium hydride, (e) reactor accessibility (transport of radioactive materials in cooling systems, ................. There have been, in addition, a number of smaller service projects, mostly of an analytical nature.:
Date: December 7, 1953
Creator: Loftness, R. L.
Object Type: Report
System: The UNT Digital Library
Process test MS-235-5, reduction of Task 3 cooling time, RM line (open access)

Process test MS-235-5, reduction of Task 3 cooling time, RM line

None
Date: January 7, 1953
Creator: Brown, C.L.
Object Type: Report
System: The UNT Digital Library
Measurements of fluctuating pressures on a 1/4-scale model of the X-1 airplane with a 10-percent-thick wing in the Langley 16-foot transonic tunnel (open access)

Measurements of fluctuating pressures on a 1/4-scale model of the X-1 airplane with a 10-percent-thick wing in the Langley 16-foot transonic tunnel

Report presenting pressure fluctuations measured near the trailing edge of the wing and near the leading edge of the tail of a scale model of the X-1 airplane with a 10-percent-thick wing in the 16-foot transonic tunnel. Results regarding frequency analyses are also provided.
Date: January 7, 1953
Creator: Habel, Louis W. & Steinberg, Seymour
Object Type: Report
System: The UNT Digital Library
Langley full-scale-tunnel tests of the Custer Channel Wing airplane (open access)

Langley full-scale-tunnel tests of the Custer Channel Wing airplane

Memorandum presenting testing of an experimental Custer Channel Wing airplane in the full-scale tunnel to investigate the lift characteristics of a channel-propeller combination and the flow phenomena in and about a channel wing.
Date: April 7, 1953
Creator: Pasamanick, Jerome
Object Type: Report
System: The UNT Digital Library
Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359 (open access)

Wind-Tunnel Investigation of the Motion of a 1/10-Scale Model of the Douglas XF4D-1 Escape Capsule When Jettisoned by Jet Ejection: TED No. NACA DE 359

Memorandum presenting a wind-tunnel investigation at low speed to determine the path and motion of a scale model of the Douglas XF4D-1 escape capsule without the drogue parachute when jettisoned by jet ejection. The investigation included determination of the vertical and horizontal accelerations of the capsule. Results regarding the ejection at zero airspeed, ejection at 570 feet per second, and at 863 feet per second are provided.
Date: October 7, 1953
Creator: Johnson, Harold S.
Object Type: Report
System: The UNT Digital Library
An investigation of three NACA 1-series nose inlets at subsonic and transonic speeds (open access)

An investigation of three NACA 1-series nose inlets at subsonic and transonic speeds

Report presenting an investigation of three NACA 1-series nose inlets at subsonic and transonic speeds in the 8-foot transonic tunnel. Drag, surface-pressure, and pressure-recovery measurements and schileren photographs were obtained at zero angle of attack through a range of Mach numbers and mass-flow-ratios. Results regarding tunnel boundary interference, surface pressure distribution, external drag, and pressure recovery are provided.
Date: January 7, 1953
Creator: Pendley, Robert E.; Milillo, Joseph R. & Fleming, Frank F.
Object Type: Report
System: The UNT Digital Library
Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model (open access)

Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model

Report presenting some equations that give the interference on the trailing-vortex system of a uniformly loaded finite-span wing in a circular tunnel containing partly open and partly closed walls, with special reference to symmetrical arrangements of the open and closed portions. Methods are given for extending the equations to include tunnel shapes other than circular.
Date: April 7, 1953
Creator: Matthews, Clarence W.
Object Type: Report
System: The UNT Digital Library
A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow (open access)

A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow

From Summary: "An analytical method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow is developed by using a simple horseshoe vortex-image system for the case of the tank axis in the plane of the wing. An illustrative example is given in the appendix, in which wing and tip-tank loadings are calculated for three configurations. The calculated results are shown to be in good agreement with experimental data."
Date: April 7, 1953
Creator: Robinson, Samuel W., Jr. & Zlotnick, Martin
Object Type: Report
System: The UNT Digital Library
The Effects of Leading-Edge Extensions, a Trailing-Edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-Fuselage-Tail Combination Having a Wing With 35 Degrees of Sweepback and an Aspect Ratio of 4.5 (open access)

The Effects of Leading-Edge Extensions, a Trailing-Edge Extension, and a Fence on the Static Longitudinal Stability of a Wing-Fuselage-Tail Combination Having a Wing With 35 Degrees of Sweepback and an Aspect Ratio of 4.5

Memorandum presenting an investigation of the leading-edge extensions, a trailing-edge extension, and a fence on the static longitudinal stability of a wing-fuselage-tail combination with a wing with 35 degrees of sweepback and an aspect ratio of 4.5. The investigation involved the use of force measurements and tuft studies on stall progression. Results regarding a model with unmodified wing, the effect of leading-edge modifications, the effects of the fence, a summary of the effects of compressibility, and some remarks on flow separation are provided.
Date: August 7, 1953
Creator: Selan, Ralph & Bandettini, Angelo
Object Type: Report
System: The UNT Digital Library
Investigation of Reynolds Number Effects for a Series of Cone-Cylinder Bodies at Mach Numbers of 1.62, 1.93, and 2.41 (open access)

Investigation of Reynolds Number Effects for a Series of Cone-Cylinder Bodies at Mach Numbers of 1.62, 1.93, and 2.41

"An investigation of the Reynolds number for transition and the skin-friction drag at zero lift of eight cone-cylinder bodies having various fineness ratios has been made at Mach numbers of 1.62, 1.93, and 2.41 over a Reynolds number range from 0.3 x 10(exp 6) to 10 x 10(exp 6). The accuracy of the skin-friction data was not sufficient to permit any general conclusions to be drawn. The Reynolds number for transition was found to be dependent upon both the tunnel stagnation pressure and Mach number" (p. 1).
Date: October 7, 1953
Creator: Grigsby, Carl E. & Ogburn, Edmund L.
Object Type: Report
System: The UNT Digital Library
A Theoretical Analysis of the Distortion of Fuel-Spray-Particle Paths in a Helicopter Ram-Jet Engine Due to Centrifugal Effects (open access)

A Theoretical Analysis of the Distortion of Fuel-Spray-Particle Paths in a Helicopter Ram-Jet Engine Due to Centrifugal Effects

Report presenting a theoretical study of certain anomalies in the behavior of a ram-jet engine engine tip-mounted on a rotating helicopter blade that appears to be related to centrifugal effects distorting the fuel-spray pattern. Results regarding the cases calculated, results of the calculations, particle-path distortion, and limiting direction of particle paths are provided.
Date: April 7, 1953
Creator: Katzoff, S. & Smith, Samuel L., III
Object Type: Report
System: The UNT Digital Library
Initial flutter tests in the Langley transonic blowdown tunnel and comparison with free-flight flutter results (open access)

Initial flutter tests in the Langley transonic blowdown tunnel and comparison with free-flight flutter results

Report presenting an experimental wing-flutter investigation in the transonic blowdown tunnel, which is equipped with a slotted test section, in order to determine the correlation between transonic-wind-tunnel and free-fall flight flutter results. Very good agreement was observed between wind tunnel and flight flutter test results, which showed the feasibility of conducting flutter tests in transonic wind tunnels with slotted test sections.
Date: January 7, 1953
Creator: Bursnall, William J.
Object Type: Report
System: The UNT Digital Library