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Rocket-Model Investigation to Determine the Hinge-Moment and Normal-Force Properties of a Full-Span, Constant-Chord, Partially Balanced Trailing-Edge Control on a 60 Degree Clipped Delta Wing Between Mach Numbers of 0.50 and 1.26

Description: Report presenting a free-flight investigation of a rocket-powered research model to determine the hinge-moment and normal-force characteristics of a trailing-edge control on a delta wing between Mach numbers of 0.50 and 1.26. The hinge-line location of 40 percent control chord satisfactorily reduced the high hinge moments associated with plain flap-type controls. Results regarding hinge moments and normal force are provided.
Date: October 30, 1953
Creator: Martz, C. William & Goslee, John W.
Partner: UNT Libraries Government Documents Department
open access

Determination of Rare Earths in Refined Uranium : Topical Report

Description: Abstract: "Rare-earth analyses were performed on several samples of refined uranium oxide and nitrate, using a modified cellulose column procedure. Rare earths were not detectable in samples of 0.03 shotgun of less. Detection limits were from 0.0005 to 0.015 ppm. Negligible quantities of low-cross-section rare earths were found in less pure uranium samples, obtained during start-up operations of the pilot plant at the Feed Materials Production Center, primarily those rare earths of greater than… more
Date: June 30, 1953
Creator: Ewing, R. A. & Bearse, A. E.
Partner: UNT Libraries Government Documents Department
open access

General Flattening and Power Curves

Description: Introduction: "In the evaluation of pile designs it is necessary to know how the production varies with the number of tubes. It has been possible to solve the problem in terms of some general parameters whose values may be quickly computed for any specific design when the pertinent information is available."
Date: March 30, 1953
Creator: Gast, Paul F.
Partner: UNT Libraries Government Documents Department

[Facts Form photograph]

Description: Photograph of a man seated in a patterned armchair. He is wearing a suit and tie. He is holding a book. He is looking to the right of the camera. A shelf with books and decorations sits against the wall in the background. There is also a side table with a lamp on it. A brick wall is to the right.
Date: April 30, 1953
Creator: WBAP-TV (Television station : Fort Worth, Tex.)
Partner: UNT Libraries Special Collections

[Photograph of Facts Form]

Description: Photograph of a man seen leaning against a desk on set and looking at the camera. The set is enclosed by fake walls with a painted backdrop featuring a door. He is wearing a dark-colored suit, a patterned tie, a white shirt, and a pocket handkerchief. Behind him, there is a framed photo mounted on the wall, a chair, a lamp, and books.
Date: April 30, 1953
Creator: WBAP-TV (Television station : Fort Worth, Tex.)
Partner: UNT Libraries Special Collections

[Margaret McDonald and Blue Birds]

Description: Photograph of Margaret McDonald and a group of girls in a kitchen. McDonald is wearing a shirt, a skirt, and accessories. Her hair is pulled into an updo. She is looking at a group of girls. The girls are wearing uniforms. There is a man visible to the right. Everyone can be seen standing behind an island in a kitchen advertised as a Youngstown Kitchen. Behind them, there is a refrigerator, a sink with a window above it, and cabinets. There are various pots, pans, and products on display. Above… more
Date: November 30, 1953
Creator: WBAP-TV (Television station : Fort Worth, Tex.)
Partner: UNT Libraries Special Collections

[Photo of WBAP-TV]

Description: Photograph of a film camera that has text on it that says "Star-Telegram WBAP-TV." There are chairs in the background and checkered tiles on the floor.
Date: September 30, 1953
Creator: WBAP-TV (Television station : Fort Worth, Tex.)
Partner: UNT Libraries Special Collections
open access

Experimental and theoretical investigation of rotating-stall characteristics of single-stage axial-flow compressor with hub-tip ratio of 0.76

Description: Report presenting the overall performance and rotating stall characteristics of a single-stage compressor with a hub-tip ratio of 0.76 and a symmetrical velocity diagram over a wide range of weight flow for several different design speed percentages. No discontinuities in performance were noted at an operating condition. Results regarding the overall performance, types of rotating stall observed, circumferential extent of stall zones, flow fluctuations incited by rotating stall, rotating-stall … more
Date: November 30, 1953
Creator: Graham, Robert W. & Prian, Vasily D.
Partner: UNT Libraries Government Documents Department
open access

Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60

Description: Report presenting an investigation to determine the effect of several seeker-nose configurations on the static longitudinal stability, canard control characteristics, and lift and drag at Mach number 1.60 of a canard-type ramjet missile with 70 degree delta canard control surfaces and 70 degree delta wings. The tests indicate that, for the most part, the configurations tested exhibited no significant difference in static longitudinal stability or horizontal-canard control effectiveness.
Date: October 30, 1953
Creator: Robins, A. Warner
Partner: UNT Libraries Government Documents Department
open access

Analysis of Heat Transfer and Fluid Friction for Fully Developed Turbulent Flow of Supercritical Water With Variable Fluid Properties in a Smooth Tube

Description: From Summary: "Calculated velocity and temperature distributions, as well as relations among Nusselt number, Reynolds number, and friction factor, are presented."
Date: January 30, 1953
Creator: Deissler, R. G. & Taylor, M. F.
Partner: UNT Libraries Government Documents Department
open access

Performance of a swept leading edge rotor of the supersonic type with mixed flow

Description: Report investigation Freon-12 as the working fluid for a 14-inch-diameter supersonic mixed-flow axial-discharge rotor of the impulse type. The whole series of tests was performed twice, once with guide vanes that underturned the air and gave a lower relative inlet velocity and once with a set that gave the design values for velocity and direction. Results regarding the overall performance characteristics, entrance flow, internal pressure patterns, exit flow, and rotor losses are provided.
Date: January 30, 1953
Creator: Goldstein, Arthur W. & Schacht, Ralph L.
Partner: UNT Libraries Government Documents Department
open access

Preliminary Investigation of a Chemical Starting Technique for the Acid - Gasoline Rocket Propellant System

Description: Memorandum presenting an investigation of the use of a small quantity of fluid that ignites spontaneously within nitric acid to initiate the acid-gasoline reaction carried out in a 200-pound-thrust uncooled engine with a characteristic length of 30 inches at a range of temperatures. The starting process was divided into two phases: ignition and transition. Results regarding ignition temperature limits, effect of temperature on allowable igniter fuel flow, optimum valve opening time for ignition… more
Date: January 30, 1953
Creator: Hennings, Glen & Morrell, Gerald
Partner: UNT Libraries Government Documents Department
open access

Force and pressure recovery characteristics at supersonic speeds of a conical spike inlet with bypasses discharging in an axial direction

Description: Report presenting an investigation of an axially symmetric nacelle-type conical spike inlet with two bypasses located in the horizontal plane and on opposite sides of the nacelle in the 8- by 6-foot supersonic tunnel at several Mach numbers and angles of attack. Results regarding the performance with open bypasses and with closed bypasses are provided.
Date: January 30, 1953
Creator: Allen, J. L. & Beke, Andrew
Partner: UNT Libraries Government Documents Department
open access

Evaluation of effects of random permeability variations on transpiration-cooled surfaces

Description: Report presenting an analytical investigation to evaluate the effects of permeability variations on surface temperatures and coolant flows for ranges of temperature and Reynolds number that are of particular interest for gas-turbine blades. Results regarding small-orifice calibrations, effect of orifices in series with porous surfaces on permeability correlation, effect of permeability variations on coolant-flow rates and porous-wall temperatures, evaluation of the experimental porous blade, an… more
Date: November 30, 1953
Creator: Esgar, Jack B. & Richards, Hadley T.
Partner: UNT Libraries Government Documents Department
open access

Comparison of theoretically and experimentally determined effects of oxide coatings supplied by fuel additives on uncooled turbine-blade temperature during transient turbojet-engine operation

Description: From Summary: "An analysis was made to permit the calculation of the effectiveness of oxide coatings in retarding the transient heat flow into turbine blades when the combustion gas temperature of a turbojet engine is suddenly changed. The analysis is checked with experimental data obtained from a turbojet engine whose blades were coated with two different coating materials (silicon dioxide and boric oxide) by adding silicone oil and tributyl borate to the engine fuel. The very thin coatings (a… more
Date: March 30, 1953
Creator: Schafer, Louis J., Jr.; Stepka, Francis S. & Brown, W. Byron
Partner: UNT Libraries Government Documents Department
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