Current Status of Longitudinal Stability (open access)

Current Status of Longitudinal Stability

The problems of static and dynamic longitudinal stability both at high speeds and at low speeds are discussed and data are presented which indicate recent progress made in the solution of these problems.
Date: May 24, 1948
Creator: Donlan, Charles J.
Object Type: Report
System: The UNT Digital Library
Current Status of Longitudinal Stability (open access)

Current Status of Longitudinal Stability

Report presenting an investigation of the problems of static and dynamic longitudinal stability both at high speeds and low speeds as well as information about progress that has been made to solve these problems. The incorporation of large amounts of sweepback on both the wing and horizontal tail can improve the rate of trim changes and stability. Longitudinal stability has been attained for configurations with a sweep angle of 45 degrees with stall-control devices, but experimental proof is needed for these devices.
Date: May 24, 1948
Creator: Donlan, Charles J.
Object Type: Report
System: The UNT Digital Library
Medical and Health Divisions quarterly report, January, February, March 1948 (open access)

Medical and Health Divisions quarterly report, January, February, March 1948

This quarterly progress report describes four programs namely (1) The Metabolic Properties of Plutonium and Allied Materials (2) Biological studies of radiation effects, (3) Biological effects of radiation from external and internal sources, and (4) Health Physics and Chemistry. Progress for each program has been separately indexed and abstracted for the database.
Date: May 24, 1948
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Preliminary investigation of hydrazine as a rocket fuel (open access)

Preliminary investigation of hydrazine as a rocket fuel

Report presenting an investigation of the properties of hydrazine, stability and corrosiveness with a number of construction materials, sensitivity to detonation and temperature, and spontaneous reaction with the oxidants, concentrated hydrogen peroxide, sodium permanganate solution, fuming nitric acid, and tetranitromethane. Results regarding corrosion and stability, sensitivity to temperature and detonation, and theoretical calculations are provided.
Date: May 24, 1948
Creator: Ordin, Paul M.; Miller, Riley O. & Diehl, John M.
Object Type: Report
System: The UNT Digital Library
Preliminary Results of British Nene II Engine Altitude-Chamber Performance Investigation. I - Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle, 1, Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle (open access)

Preliminary Results of British Nene II Engine Altitude-Chamber Performance Investigation. I - Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle, 1, Altitude Performance Using Standard 18.75-Inch-Diameter Jet Nozzle

An investigation is being conducted to determine the altitude performance characteristics of the British Nene II engine and its components. The present paper presents the preliminary results obtained using a standard jet nozzle. The test results presented are for conditions simulating altitudes from sea level to 60,000 feet and ram pressure ratios from 1.0 to 2.3. These ram pressure ratios correspond to flight Mach numbers between zero and 1.16 assuming a 100 percent ram recovery.
Date: May 24, 1948
Creator: Barson, Zelmar & Wilsted, H. D.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-585 (open access)

Texas Attorney General Opinion: V-585

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: Time limitation, if any, before an election to incorporate a school district may follow an election which abolished an independent school district.
Date: May 24, 1948
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Visual Observations of the Shock Wave in Flight (open access)

Visual Observations of the Shock Wave in Flight

"This report presents the results of pilot observations and photographs of the compression shock wave on the wing of an airplane in flight. A detailed description of the test conditions necessary and the procedure to be following in producing the visible shock are presented. The pilot's observations of the occurrence of an oscillating shock wave and its possible relationship with the airplane buffeting are also presented" (p. 1).
Date: May 24, 1948
Creator: Cooper, George E. & Rathert, George A., Jr.
Object Type: Report
System: The UNT Digital Library