Analysis of an automatic control to prevent rolling divergence (open access)

Analysis of an automatic control to prevent rolling divergence

From Introduction: "The use of automatic controls to reduce the tendency for rolling divergence has been investigated in references 2 and 3. These studies have considered the effect of artificial changes in certain stability derivatives on the rolling divergence, and have shown that increased damping in pitch may be quite effective in reducing the divergent tendency. In the present report, a different type of automatic control is investigated."
Date: April 18, 1956
Creator: Phillips, William H.
System: The UNT Digital Library
Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing (open access)

Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing

Report presenting force-test data showing the effects of change in leading-edge radius on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing of aspect ratio 3 for several ranges of Mach and Reynolds numbers. The results indicated that as the airfoil sections were thinned at the nose, separation effects occurred at lower values of lift coefficient.
Date: April 18, 1956
Creator: Schneider, William C.
System: The UNT Digital Library
An evaluation of an aeromechanical method of minimizing servo- missile transfer function variations with flight condition (open access)

An evaluation of an aeromechanical method of minimizing servo- missile transfer function variations with flight condition

Report presenting a theoretical investigation to determine the static and dynamic characteristics of a control-surface actuator and missile combination, with primary consideration given to the minimization of the effects of Mach number and altitude.The results indicate that the type of actuator studied in combination with a missile might replace a gain-adjusted acceleration control system. Results regarding the control-system static characteristics, control-system dynamic characteristics, comparison of torposervo and position-servo actuation, and some suggestions for further research are provided.
Date: April 18, 1956
Creator: Nason, Martin L.
System: The UNT Digital Library
The Extrusion of Composite Tubes, SPEECH for AEC Metallurgical Information Meeting, Ames, Iowa 2-4 (open access)

The Extrusion of Composite Tubes, SPEECH for AEC Metallurgical Information Meeting, Ames, Iowa 2-4

None
Date: April 18, 1956
Creator: D' Amore, M. R. & Inouye, H.
System: The UNT Digital Library
Flight measurements of horizontal-tail loads on the Douglas X-3 research airplane (open access)

Flight measurements of horizontal-tail loads on the Douglas X-3 research airplane

Report presenting flight measurements of the horizontal-tail loads on the Douglas X-3 research airplane during wind-up turns, pull-ups, and stabilizer pulses over a range of altitudes and Mach numbers.
Date: April 18, 1956
Creator: Stephenson, Harriet J.
System: The UNT Digital Library
HRT COOLING-WATER SYSTEM. HRT Engineering Test Procedures VI A-2, 3, 4, 5 B-1, a, b B-2 and B-3 (open access)

HRT COOLING-WATER SYSTEM. HRT Engineering Test Procedures VI A-2, 3, 4, 5 B-1, a, b B-2 and B-3

Experimental procedures for testing the HRT coolingwater system and its components are presented. The cooling-water system is a closed system consisting of three parallel circuits fed by a single circulating pump fed from a forced draft cooling tower and supply reservoir. In the event of radioactive contamination of the cooling-water system the tower supply lines are equipped with block valves that confine the solutions to the reactor cell, and after shutdown heat may be removed by discharging contaminated cooling water to the cell. Failure of the circuevert of radioactive contamination of the cooling- water system the tower supply lines are equipped with block valves that confine the solutions to the reactor cell, and after shutdown heat may be removed by discharging contaminated cooling water to the cell. Failure of the circulating pump will actuate a valve that will permit convection cooling to take place within a closed circuit. (auth)
Date: April 18, 1956
Creator: Brooksbank, R.E.
System: The UNT Digital Library
PROCEDURE FOR PERFORMANCE TEST OF TURBINE CONDENSER AND ASSOCIATED EQUIPMENT. HRT Test V A 2, a, b, c (open access)

PROCEDURE FOR PERFORMANCE TEST OF TURBINE CONDENSER AND ASSOCIATED EQUIPMENT. HRT Test V A 2, a, b, c

None
Date: April 18, 1956
Creator: Kolb, J.O. & Brooksbank, R.E.
System: The UNT Digital Library
Savannah River Plant, Works Technical Department monthly progress report for March 1956 (open access)

Savannah River Plant, Works Technical Department monthly progress report for March 1956

This document details activities of the Works Technical Department during the month of March 1956. It covers reactor technology, separations technology, engineering assistance and heavy water technology.
Date: April 18, 1956
Creator: unknown
System: The UNT Digital Library
THOREX PILOT PLANT: DECONTAMINATION RUN IX-16 (open access)

THOREX PILOT PLANT: DECONTAMINATION RUN IX-16

None
Date: April 18, 1956
Creator: Walker, J.H. & Sadowski, G.S.
System: The UNT Digital Library