Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations (open access)

Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations

From Introduction: "This report makes further comparisons of the theoretical computing method with available experimental results, showing effects of wing plan-form changes, and the effect of an airfoil-section change on a wing of given plan form."
Date: August 15, 1955
Creator: Holdaway, George H.
Object Type: Report
System: The UNT Digital Library
An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface (open access)

An experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface

Report presenting the results of an experimental investigation of the unsteady lift induced on a wing in the downwash field of an oscillating canard control surface. The results indicated that existing theories provide a reliable guide for the estimation of the magnitude of the lift derivatives and centers of pressure at low values of reduced frequency and low angles of attack.
Date: August 15, 1955
Creator: Reese, David E., Jr.
Object Type: Report
System: The UNT Digital Library
The Kinetics of the Zirconium-Uranium Dioxide Reaction (open access)

The Kinetics of the Zirconium-Uranium Dioxide Reaction

This report discusses three experimental methods used to study the kinetics of the reaction between zirconium and UO2.
Date: August 15, 1955
Creator: Mallett, Manley William, 1909-; Gerds, Arnold F.; Lemmon, Alexis W. & Chase, Dan L.
Object Type: Report
System: The UNT Digital Library
THE KINETICS OF THE ZIRCONIUM-URANIUM DIOXIDE REACTION (open access)

THE KINETICS OF THE ZIRCONIUM-URANIUM DIOXIDE REACTION

None
Date: August 15, 1955
Creator: Mallett, M.W.; Gerds, A.F.; Lemmon, A.W. & Chase, D.L.
Object Type: Report
System: The UNT Digital Library
Minutes of Technical Division Steering Committee meeting August 9, 1955, Savannah River Laboratory (open access)

Minutes of Technical Division Steering Committee meeting August 9, 1955, Savannah River Laboratory

Study approvals are listed for Studies 8506, 8509, 8518, 8519, and 8520 with man-months and program dates specified. Safety and security agreements are listed. Additional topics discussed are: financial status, experimental physics programs, pile engineering division program, and technical division study status.
Date: August 15, 1955
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Monthly report - Process Section, Manufacturing Division, July 1955 (open access)

Monthly report - Process Section, Manufacturing Division, July 1955

This document is the July 1955 Monthly Report of the Process Section/Manufacturing Division at the Savannah River Plant. It contains information on activities in each of the SRP areas (100-400 areas), as well as on utilities and general services.
Date: August 15, 1955
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Quarterly progress report, Metallurgy Research sub-section, April 1955--June 1955 (open access)

Quarterly progress report, Metallurgy Research sub-section, April 1955--June 1955

One uranium tensile specimen irradiated to 620 MWD/T (1.75 x 10{sup 20} nvt) was tested at 285 C (545 F). The values obtained were: ultimate tensile strength 71,000 psi, 0.1% offset yield strength 70,000 psi, percent elongation (one inch gage length) 0.7, and modulus of elasticity 12 x 10{sup 6}. These values are comparable to the as-irradiated values of specimens tested at room temperature which were: ultimate tensile strength 76,000 psi, 0.1% offset yield strength 71,500 psi, and percent elongation (one inch gage length) 0.36. The elongation of the specimen tested at 285 C was less than that of a specimen annealed at 700 C (1290 F) after irradiation, then tested at room temperature. Experiments have been initiated to determine the structural stability of irradiated uranium-silicon alloy when this alloy is in the stable epsilon phase. Present work is limited to the evaluation of thermal expansion as a criterion for degree of epsilonization. This technique has not proven satisfactory. The damage resulting from the bombardment of uranium with electrons in the 1-2 MEV range is to be evaluated using electrical resistivity and x-ray diffraction to determine the extent of the damage. Calculations indicate a threshold energy of about 1.25 MEV …
Date: August 15, 1955
Creator: Cadwell, J.J.
Object Type: Report
System: The UNT Digital Library
A Simultaneous Scaler Control System (open access)

A Simultaneous Scaler Control System

The primary purpose of this writeup is to present a description of the electrical and mechanical features of the developed system for use in maintenance and operation of a simultaneous scaler control unit.
Date: August 15, 1955
Creator: Tomlinson, R. L.
Object Type: Report
System: The UNT Digital Library
Some aspects of the design of hypersonic boost-glide aircraft (open access)

Some aspects of the design of hypersonic boost-glide aircraft

Report discussing factors influencing flight range and aerodynamic heating for hypersonic boost-glide aircraft. The possibility and advantages of flight at very high altitude to reduce aerodynamic heating and encourage the preservation of laminar flow on the surface of the aircraft is explored.
Date: August 15, 1955
Creator: Seiff, Alvin & Allen, H. Julian
Object Type: Report
System: The UNT Digital Library
Static Longitudinal and Lateral Stability and Control Characteristics of an Airplane Configuration Having a Wing of Trapezoidal Plan Form With Various Tail Airfoil Sections and Tail Arrangements at a Mach Number of 6.86 (open access)

Static Longitudinal and Lateral Stability and Control Characteristics of an Airplane Configuration Having a Wing of Trapezoidal Plan Form With Various Tail Airfoil Sections and Tail Arrangements at a Mach Number of 6.86

Memorandum presenting an investigation carried out in the 11-inch hypersonic tunnel to determine the static longitudinal and lateral stability and control characteristics of an airplane configuration with a trapezoidal wing with a modified hexagonal airfoil section and equipped with various tail airfoil sections and tail arrangements. The tests were made at Mach number 6.86 and Reynolds number 343,000 based on the wing mean aerodynamic chord.
Date: August 15, 1955
Creator: Penland, Jim A.; Fetterman, David E., Jr. & Ridyard, Herbert W.
Object Type: Report
System: The UNT Digital Library
A study of service-imposed maneuvers of four jet fighter airplanes in relation to their handling qualities and calculated dynamic characteristics (open access)

A study of service-imposed maneuvers of four jet fighter airplanes in relation to their handling qualities and calculated dynamic characteristics

Report presenting results from a flight program conducted to obtain information on the airplane response and actual rates and amounts of control motion used by service pilots to perform squadron operational training missions, which are correlated with the airplane handling qualities and calculated maximum dynamic response. Results regarding longitudinal characteristics, rolling characteristics, and sideslip characteristics are provided.
Date: August 15, 1955
Creator: Mayer, John P. & Hamer, Harold A.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: MS-231 (open access)

Texas Attorney General Opinion: MS-231

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; Expiration of appropriation to State Board of Veterinary Medical Examiners under Article 7465-a, Vernon's Civil Statutes.
Date: August 15, 1955
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History