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Effects of Some Present-Day Airplane Design Trends on Requirements for Lateral Stability

Description: Note presenting computations made to determine the effects of some airplane design trends on the fin area and the dihedral angle required for lateral stability. The specific factors studied were wing loading, moments of inertia in roll and yaw, wing chord, and tail length. The results of the computations are presented in the form of diagrams of variations of fin area with dihedral angle for neutral stability.
Date: June 1941
Creator: Bamber, Millard J.
Partner: UNT Libraries Government Documents Department
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Use of Brine in a Kansas Field for Secondary Recovery of Oil

Description: Report issued by the U.S. Bureau of Mines on the use of oil field brine in secondary recovery methods. Characteristics of the brine, and methods used in recovery processes are presented. This report includes tables, graphs, maps, and illustrations.
Date: June 1941
Creator: Wilhelm, C. J.; Taylor, Sam S.; Holliman, W. C. & Owens, E. O.
Partner: UNT Libraries Government Documents Department

[Gilbert Dove shaves for his wedding(2)]

Description: Photograph of Gilbert Dove shaving in front of a mirror before his wedding to Hazel Petrey. Printed on the matte is text that reads, "Gilbert shaves before the wedding". This mounted print is from a book entitled, "Country Wedding". Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the story “Life Magazine Goes to a Kentucky Wedding.” Also in the Joe Clark, HSSS book “Country Wedding" published in 1974. Additionall… more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections

[Bride and groom on their way to the church]

Description: Photograph of Hazel Petrey and Gilbert Dove walking to the Sunny View Methodist Church (visible in the top right corner) to rehearse their wedding. The flower girl, Hazel's younger sister Anna Ruth Petrey, walks with them. The words "...and up the main road to the church" are written on the matte. This mounted print is from a book entitled, "Country Wedding". Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the s… more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections

[Gilbert Dove dresses for his wedding(1)]

Description: Photograph of Gilbert Dove getting dressed on the day of his wedding to Hazel Petrey. This mounted print is from a book entitled, "Country Wedding". Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the story “Life Magazine Goes to a Kentucky Wedding.” Also in the Joe Clark, HSSS book “Country Wedding" published in 1974. Additionally a 1982 photo of Hazel and Gilbert can be found in Joe’s Tennessee Scrapbook. All ar… more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections

[Hazel Petrey cooking breakfast on her wedding day(2)]

Description: Photograph of Hazel Petrey cooking breakfast in her kitchen the morning of her wedding to Gilbert Dove. She makes eggs in a skillet on her Supreme Enterprise stove and there is a plate of biscuits to her right. There is text printed on the mat along the bottom of the photo. This mounted print is from a book entitled, "Country Wedding." Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the story “Life Magazine Goes … more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections

[Happily ever after]

Description: Photograph of a sign that reads, "...and They Lived Happily Ever After" in a decorative font. This matted image was the final in the Country Wedding series photographed by Joe Clark. Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the story “Life Magazine Goes to a Kentucky Wedding.” Also in the Joe Clark, HSSS book “ Country Wedding published in 1974. Additionally a 1982 photo of Hazel and Gilbert can be found in … more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections
open access

Chemical Properties of Uranium Hexafluoride, UF6

Description: Uranium hexafluoride has the distinction of being the only stable gaseous compound of uranium known up to the present moment. Because of this property it is the only compound that can be used for processes of isotope separation, such as diffusion, thermal diffusion, centrifuge separation, distillation, and other of a similar nature. Here is a short description of the properties of UF{sub 6} and is intended for a reader interested only casually in this compound. UF{sub 6} is a very reactive comp… more
Date: June 25, 1941
Creator: Grosse, Aristid V.
Partner: UNT Libraries Government Documents Department
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Wind-tunnel investigation of control-surface characteristics 1: effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap

Description: From Summary: "Tests have been made to determine the effect of a gap at the flap nose upon the aerodynamic section characteristics of an NACA 0009 airfoil with a plain flap and tab. The results are presented in the form of airfoil and flap section characteristics for several flap deflections, tab deflections, and for four sizes of gap."
Date: June 1941
Creator: Sears, Richard I.
Partner: UNT Libraries Government Documents Department
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Wind-tunnel investigation of an NACA 23012 airfoil with a 30 percent chord Maxwell slate and with trailing-edge flaps

Description: Report presenting an investigation in the 7- by 10-foot wind tunnel of an NACA 23012 airfoil with a 30 percent-chord Maxwell leading-edge slat and a slotted and a split flap. The main purpose was to determine the optimum slot cap of the Maxwell slat for, and the aerodynamic section characteristics of, the airfoil with several deflections for both types of flaps. Curves of lift, drag, and pitching-moment characteristics for optimum arrangements are provided.
Date: June 1941
Creator: Lowry, John G. & McKee, John W.
Partner: UNT Libraries Government Documents Department
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Wind-Tunnel Investigation of a Plain and a Slot-Lip Aileron on a Wing With a Full-Span Flap Consisting of an Inboard Fowler and an Outboard Slotted Flap

Description: Report presenting an investigation of a slot-lip aileron and a plain aileron, singly and in combination, on an NACA 23012 wing with a full-span flap. The characteristics of these lateral-control devices were essentially the same as those of similar devices on the wing with full-span NACA slotted flaps as tested in a previous investigation.
Date: June 1941
Creator: Rogallo, F. M. & Schuldenfrei, Marvin
Partner: UNT Libraries Government Documents Department

[Hazel Petrey cooking breakfast on her wedding day(1)]

Description: Photograph of Hazel Petrey cooking breakfast in her kitchen the morning of her wedding to Gilbert Dove. She makes eggs in a skillet on her Supreme Enterprise stove and there is a plate of biscuits to her right. Narrative by Junebug Clark: More images and information can be found in the July 28, 1941 issue of Life Magazine, pages 82-85 in the story “Life Magazine Goes to a Kentucky Wedding.” Also in the Joe Clark, HSSS book “ Country Wedding published in 1974. Additionally a 1982 photo of Hazel … more
Date: June 15, 1941
Creator: Clark, Joe
Partner: UNT Libraries Special Collections
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The theoretical lateral motions of an automatically controlled airplane subjected to a yawing moment disturbance

Description: Report presenting an investigation of the lateral motion resulting from a disturbance of the type produced by asymmetric loss of thrust for a hypothetical average airplane equipped with an automatic pilot. Plots of the resultant motion and various modes that constitute the motion are presented for fixed controls and for various amounts of autopilot.
Date: June 1941
Creator: Imlay, Frederick H.
Partner: UNT Libraries Government Documents Department
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Cooling Effects of an Airplane Equipped With an NACA Cowling and a Wing-Duct Cooling System

Description: Report presenting cooling tests of a Northrop A-17A attack airplane equipped with a conventional NACA cowling and then with a wing-duct cooling system. Ground cooling for the wing-duct system without cowl flap was better than for the cowling with flap, but was improved by installing a cowl flap. Satisfactory temperatures were maintained in climb and high-speed flight, but a greater quantity of cooling air was needed for the wing-duct system.
Date: June 1941
Creator: Turner, L. I., Jr.; Bierman, David & Boothby, W. B.
Partner: UNT Libraries Government Documents Department
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Preliminary Stability and Control Tests in the NACA Free-Flight Wind Tunnel and Correlation With Full-Scale Flight Tests

Description: Note presenting a study of stability and control of airplanes by means of dynamic scale models in the 12-foot free-flight wind tunnel. Tests of a scale model of the F-36A airplane were used to develop the testing technique and to afford a comparison of tests of a model in the tunnel with flight tests of the corresponding airplane. Results regarding longitudinal stability and control and lateral stability and control are provided.
Date: June 1941
Creator: Shortal, Joseph A. & Osterhout, Clayton J.
Partner: UNT Libraries Government Documents Department
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The Effect of Methods of Testing on the Ultimate Loads Supported by Stiffened Flat Sheet Panels Under Edge Compression

Description: Note presenting testing of two series of stiffened flat sheet specimens tested under edge compression using various end conditions: round ends, flat ends, and continuous panels. The specimens consisted of aluminum-alloy flat sheet stiffened by three hat-shaped extruded aluminum-alloy stiffeners. The results indicated that the length of the specimen has an insignificant effect on the ultimate compressive load.
Date: June 1941
Creator: Holt, Marshall
Partner: UNT Libraries Government Documents Department
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Power-off wind-tunnel tests of the 1/8-scale model of the Brewster F2A airplane

Description: "At the request of the Bureau of Aeronautics, Navy Department, tests were made in the 7- by 10-foot wind tunnel of the 1/8-scale model of the Brewster F2A airplane. The object of the tests was to determine the power-off static lateral and longitudinal stability and control of the complete model" (p. 1).
Date: June 1941
Creator: Lowry, John G.
Partner: UNT Libraries Government Documents Department
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An analytical study of wing and tail loads associated with an elevator deflection

Description: From Introduction: "The present paper covers step 1 of the outlined investigation, includes methods of computing the variation of wing and tail loads, and gives numerical results of the application of the theory to the BT-9B airplane. Finally, theoretical formulas are developed and charts are given for computing the maximum increments of wing load, the down-tail load, and the up-tail load following a given elevator displacement."
Date: June 1941
Creator: Pearson, H. A. & Garvin, J. B.
Partner: UNT Libraries Government Documents Department

"Arise Americans" : your country and your liberty are in grave danger -- protect them now by joining the-- United States Navy or the U.S. Naval Reserve.

Description: A sailor in a white uniform uses a wrench on a large weapon or equipment. A blue border with white stars surrounds the top and sides of the picture. The bottom half of the poster is red, with white and blue text.
Date: June 18, 1941
Creator: Barclay, McClelland.
Partner: UNT Libraries Government Documents Department
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A Flight Investigation of the Thermal Properties of an Exhaust Heated Wing De-Icing System on a Lockheed 12-A Airplane

Description: "The thermal properties are presented for the exhaust heated wing de-icing system of a Lockheed 12-A airplane which has successfully prevented a wing icing in 25 hours of flying in various icing conditions. The quantities of heat supplied for de-icing of the wings under various conditions were measured and are presented. The distribution of temperatures above the ambient air temperature for the wing surface under various operating conditions are given" (p. 1).
Date: June 1941
Creator: Rodert, Lewis A. & Clousing, Lawrence A.
Partner: UNT Libraries Government Documents Department
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