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Results of transient and steady state experiments investigating hazards of flow reductions in a K process tube (open access)

Results of transient and steady state experiments investigating hazards of flow reductions in a K process tube

The purpose of this report is to present the results of transient and steady state heat transfer experiments investigating the degree of protection offered by the Panellit pressure gage system to hazards arising from coolant flow reductions to a K process tube.
Date: January 2, 1958
Creator: Hesson, G. M. & Thorne, W. L.
System: The UNT Digital Library
Viscosities and Densities of Methanol-Toluene Solutions up to their Normal Boiling Points (open access)

Viscosities and Densities of Methanol-Toluene Solutions up to their Normal Boiling Points

Report on an experiment to determine the boiling point values of methanol-toluene solutions, with a focus on the viscosity and density of the solution. Includes tables and findings.
Date: January 2, 1958
Creator: Hammond, L. W.; Howard, Katherine S. & McAllister, R. A.
System: The Portal to Texas History
Wind-Tunnel Investigation of the Low-Speed Characteristics of a 1/8-Scale Model of the Republic XP-91 Airplane with a Vee and a Conventional Tail. Addendum - Characteristics with a Revised Conventional Tail and Drooped Wing Tips (open access)

Wind-Tunnel Investigation of the Low-Speed Characteristics of a 1/8-Scale Model of the Republic XP-91 Airplane with a Vee and a Conventional Tail. Addendum - Characteristics with a Revised Conventional Tail and Drooped Wing Tips

"Additional wind-tunnel tests were made of a 1/8-scale model of the Republic XP-91 airplane to determine its characteristics with various modifications. The modifications included a revised conventional tail, revised rocket arrangement, drooped wing tips, and revised landing gear and doors. Tests were also made to determine the effectiveness of the control surfaces of the model with the conventional tail and the effect of changing wing incidence and tail length. The revised rocket arrangement provided a considerable increase in the static directional stability contributed by the vee tail at small angles of yaw" (p. 1).
Date: January 2, 1958
Creator: Weiberg, James A. & Anderson, Warren E.
System: The UNT Digital Library