You limited your search to:

 Collection: Technical Report Archive and Image Library
Starting and performance characteristics of a large asymmetric supersonic free-jet facility

Starting and performance characteristics of a large asymmetric supersonic free-jet facility

Date: April 1, 1954
Creator: Seashore, Ferris, L & Hurrell, Herbert G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Starting characteristics and combustion performance of magnesium slurry in 6.5-inch-diameter ram-jet engine mounted in connected-pipe facility

Starting characteristics and combustion performance of magnesium slurry in 6.5-inch-diameter ram-jet engine mounted in connected-pipe facility

Date: January 28, 1954
Creator: Gibbs, James B
Description: The starting characteristics and combustion performance of slurry type fuels, consisting of 50 percent magnesium powder in a hydrocarbon carrier, have been investigated in a flight-type, 6.5-inch-diameter ram-jet engine in a connected-pipe facility. Quick, dependable starting of the engine was obtained by the use of a disk which blocked part of the combustor area downstream of the flame holder. Acceptable performance was achieved with a short fuel-air mixing length by the development of a fuel-distribution control sleeve.
Contributing Partner: UNT Libraries Government Documents Department
Startup Operation of a Production Facility for Separating Barium-140 from MTR Fuel

Startup Operation of a Production Facility for Separating Barium-140 from MTR Fuel

Date: September 1, 1957
Creator: Legler, Billy Mason; Fairbourne, S. F.; Kelly, P. N. & Robinson, R. A.
Description: Report describing "the startup operation of a batch production facility for separating and purifying barium-140 from short-cooled MTR fuel" (p. 3).
Contributing Partner: UNT Libraries Government Documents Department
State and development of flutter calculation

State and development of flutter calculation

Date: March 1, 1951
Creator: Teichmann, Alfred
Description: This report discusses the need for considering a wide variation in certain of the basic flutter parameters in conducting a flutter analysis. Conclusions are drawn stating that design charts or simple rules may be misleading. Due to inherent difficulties, dynamic model testing may also yield misleading results. The general flutter equations and various methods of solution are discussed. Of particular interest, curves are presented showing computational effort plotted against a number of degrees of freedom used in a flutter analysis.
Contributing Partner: UNT Libraries Government Documents Department
State Compensatory Provisions for Occupational Diseases

State Compensatory Provisions for Occupational Diseases

Date: unknown
Creator: Morgis, G. G.; Beauregard, Lena P. & Shoub, Earle P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
State-of-the-Art Review of Materials-Related Problems in Flue Gas Desulfurization Systems

State-of-the-Art Review of Materials-Related Problems in Flue Gas Desulfurization Systems

Date: October 1980
Creator: Maiya, P. S.
Description: This report characterizes the chemical and mechanical environments to which the structural components used in flue-gas desulfurization (FGD) are exposed. It summarizes the necessary background information pertinent to various FGD processes currently in use, with particular emphasis on lime/limestone scrubbing technology, so that the materials problems and processing variables encountered in FGD systems can be better defined and appreciated. The report also describes the materials currently used and their performance to date in existing wet scrubbers. There is little doubt that with more extensive use of coal and flue-gas scrubbers by utilities and other segments of private industry, a better understanding of the material failure mechanisms, performance limitations, and potential problem areas is required for the design of more reliable and cost-effective FGD systems.
Contributing Partner: UNT Libraries Government Documents Department
Static aeroelastic phenomena of M-, W-, and A-wings

Static aeroelastic phenomena of M-, W-, and A-wings

Date: February 9, 1953
Creator: Diederich, Franklin W & Foss, Kenneth A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static and dynamic creep properties of laminated plastics for various types of stress

Static and dynamic creep properties of laminated plastics for various types of stress

Date: February 1, 1947
Creator: Marin, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The static and dynamic-rotary stability derivatives at subsonic speeds of a model of the X-15 research airplane

The static and dynamic-rotary stability derivatives at subsonic speeds of a model of the X-15 research airplane

Date: September 15, 1958
Creator: Lopez, Armando E & Tinling, Bruce E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The static and dynamic-rotary stability derivatives at subsonic speeds of an airplane model with an unswept wing and a high horizontal tail

The static and dynamic-rotary stability derivatives at subsonic speeds of an airplane model with an unswept wing and a high horizontal tail

Date: January 14, 1957
Creator: Buell, Donald A; Reed, Verlin D & Lopez, Armando E
Description: None
Contributing Partner: UNT Libraries Government Documents Department