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[Byrd III and Byrd IV with cameras]

Description: Edited photograph of Byrd III and Byrd IV holding cameras that are pointed at one another. The camera that Byrd III is holding is a Bolex movie camera. They are both wearing long-sleeve, button-up shirts with ties. The original photograph included only Byrd III, but Byrd IV edited the photograph to include himself.
Date: {1936,2011}
Creator: Williams, Byrd M. (Byrd Moore), IV, 1951-
Item Type: Refine your search to only Photograph
Partner: UNT Libraries Special Collections

[Photo of a girl playing guitar]

Description: Photograph of a girl sitting by a window with lacy curtains, playing guitar. Behind her is a wall covered in catalog papers and a calendar. In the corner is a standing mirror. The photo is accompanied by a poem called "Four Maidens".
Date: {1939..1989,1961-11-07}
Creator: Clark, Joe
Item Type: Refine your search to only Photograph
Partner: UNT Libraries Special Collections

[Photograph of Byrd and Mary Williams near the water]

Description: Photograph of Byrd Williams Sr and his wife, Mary Williams, sitting on a rocky shore near a body of water in a ravine. Byrd sits on the left, wearing a long jacket over a suit. He holds a brimmed hat at his side. Mary wears a long dress, a bonnet, and a string of beads. A closed fan rests in her lap. The water behind them crashes. In the background, a high bridge stretches across the water.
Date: [..1932]
Item Type: Refine your search to only Photograph
Partner: UNT Libraries Special Collections
open access

[Letter to Hortensia Blanca Mariajiminez from Santiago L. Jaurez]

Description: Letter to Hortensia Blanca Mariajiminez from Santiago L. Jaurez. A large eagle icon is printed next to names and titles that are positioned above a line. Below the line is a title and a date centered above a column of paragraphed text. A signature has been marked below the text column.
Date: December 9, 1939
Creator: Parlee, Lorena, 1945-2006 & Jaurez, Santiago L.
Item Type: Refine your search to only Text
Partner: UNT Libraries Special Collections
open access

The Breda Wind Tunnel

Description: A description of the design and construction of the Breda wind tunnel. The tunnel is equipped with a two-meter throat diameter and a 310 kph velocity potential.
Date: December 1939
Creator: Pittoni, Mario
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Contribution to the Aerodynamics of Rotating-Wing Aircraft

Description: "The chief defect of the investigations up to now was the assumption of a more or less arbitrary "mean" drag coefficient for a section of the blade. This defect is remedied through replacement of the constant coefficient by a function of higher order which corresponds to the polar curve of the employed profile. In that way it is possible to extend the theory to include the entire range from "autogyro" without power input to the driven "helicopter" with forward-tilted rotor axis. The treatment i… more
Date: December 1939
Creator: Sissingh, G.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

The Effect of Streamlining the Afterbody of an N.A.C.A. Cowling

Description: "The drag and the power cost associated with the changing of the nose of a nacelle from a streamline shape to a conventional N.A.C.A. cowling shape was investigated in the N.A.C.A. 20-foot tunnel. Full-scale propellers and nacelles were used. The increment of drag associated with the change of nose shapes was found to be critically dependent on the afterbody of the nacelle" (p. 1).
Date: December 1939
Creator: Stickle, George W.; Crigler, John L. & Naiman, Irven
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

The Effect of Streamlining the Aterbody of an N.A.C.A. Cowling

Description: Report presenting an investigation of the drag and power cost associated with the changing of the nose of a nacelle from a streamline shape to a conventional cowling shape. Full-scale propellers and nacelles were used. The results of the tests showed that the streamline afterbody drag approached that of an airship form and that the added drag due to the open-nose cowling was only a quarter of the drag increase obtained with the other afterbody.
Date: December 1939
Creator: Stickle, George W.; Crigler, John L. & Naiman, Irven
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Liquefied Gas for the Household.

Description: Describes the benefits of using liquefied gas as a means of power in the home, how it is measured and distributed, and its comparative costs.
Date: December 1939
Creator: Senner, Arthur H. (Arthur Henry) & Holbrook, Helen S. (Helen Shepard), b. 1882
Item Type: Refine your search to only Book
Partner: UNT Libraries Government Documents Department
open access

Local instability of columns with I-, Z-, channel, and rectangular-tube sections

Description: From Summary: "Charts are presented for the coefficients in the formulas for the critical compressive stress at which cross-sectional distortion begins in thin-wall columns of I-, Z-, channel, and rectangular-tube sections. The energy method of Timoshenko was used in the theoretical calculations required for the construction of the charts. The deflection equations were carefully selected to give good accuracy. The calculation of the critical compressive stress at stresses above the elastic rang… more
Date: December 1939
Creator: Stowell, Elbridge Z. & Lundquist, Eugene E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Modern Methods of Testing

Description: After a brief survey of the commonly used single-value test methods, the importance of the determination of the incipient knock for the octane number is discussed and improvements suggested for the knock testing in the CFR engine. The DVL supercharge test method with its superiority of direct determination of fuel knock in each single cylinder of an airplane engine without involving structural changes, is described and the advantages of a multiple-value method enumerated. A diagrammatic present… more
Date: December 1939
Creator: Seeber, F.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Observations in Flight of the Region of Stalled Flow Over the Blades of an Autogiro Rotor

Description: "The flow over the inner halves of the rotor blades on a Kellet YG-1B autogiro was investigated in flight by making camera records of the motion of silk streamers attached to the upper surfaces of the blades. These records were analyzed to determine the boundaries of the region within which the flow over the blade sections was stalled for various tip-speed ratios. For the sake of comparison, corresponding theoretical boundaries were obtained. Both the size of the stalled area and its rate of gr… more
Date: December 1939
Creator: Bailey, F. J., Jr. & Gustafson, F. B.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Pressure-Distribution Measurements on a Rectangular Wing With a Partial-Span Split Flap in Curved Flight

Description: "Pressure-distribution tests were made on the 32-foot whirling arm of the Daniel Guggenheim Airship Institute of a rectangular wing of NACA 23012 section to determine the rolling and the yawing moment due to angular velocity in yaw. The model was tested at 0 and 5 degree pitch; 0, +/- 5, and +/- 10 degrees yaw; and with no flap and with split flaps 25, 50 and 75 percent of the wing span and deflected 60 degrees. The results are given in the form of span load distributions and as calculated mome… more
Date: December 1939
Creator: Rokus, Frank G.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Profile-Drag Investigation of an Airplane Wing Equipped with Rubber Inflatable De-Icer

Description: "The National Advisory Committee for Aeronautics has made profile-drag measurements in flight of a wing which was equipped with a rubber inflatable de-icer and to which various stimulated ice formations were attached. Tuft observations at the stalling speed of the wing with the various drag conditions were made in order to determine the influence on the maximum lift coefficient. The de-icer installation caused an increase of from 10-20% in the profile drag of the plain wing and reduced CL(sub m… more
Date: December 1939
Creator: Rodert, Lewis A. & Jones, Alun R.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Protecting Field Borders.

Description: A guide to establishing borders for farm fields, in order to allow for drainage, to prevent woodland encroachment, and to provide wildlife protection.
Date: December 1939
Creator: Davison, Verne E. (Verne Elbert), 1904-
Item Type: Refine your search to only Book
Partner: UNT Libraries Government Documents Department
open access

A Recurrence Formula for Shear-Lag Problems

Description: "The analysis of the bending action in box beams with appreciable shear deformation of the flanges becomes very difficult in the general case of variable cross section and loading. This paper presents a convenient method of solving the problem by the familiar method of dividing the beam into a number of bays that can be assumed to have constant cross section and loading. Application of formerly derived shear-lag formulas leads to a general equation closely analogous in form to the well-known th… more
Date: December 1939
Creator: Kuhn, Paul
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Stress concentration around an open circular hole in a plate subjected to bending normal to the plane of the plate

Description: "An aluminum-alloy plate containing an open circular hole of diameter large compared with the thickness of the plate was subjected to bending forces normal to the plane of the plate. Deflection and strain measurements were taken for two different loads. Stress concentrations occurred at the edge of the hole and the maximum stresses were tangential to the hole at the ends of the transverse diameter. The maximum stress at the edge of the hole was 1.59 times the computed stress on the net section … more
Date: December 1939
Creator: Dumont, C.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Effect of fuel-air ratio, inlet temperature, and exhaust pressure on detonation

Description: From Summary: "An accurate determination of the end-gas condition was attempted by applying a refined method of analysis to experimental results. The results are compared with those obtained in Technical Report no. 655. The experimental technique employed afforded excellent control over the engine variables and unusual cyclic reproducibility. This, in conjunction with the new analysis, made possible the determination of the state of the end-gas at any instant to a fair degree of precision. Resu… more
Date: November 15, 1939
Creator: Taylor, E. S.; Leary, W. A. & Diver, J. R.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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