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[Letter from James Stuart to L. Moore, November 4, 1832]

Description: Letter from James Stuart to L. Moore. In the letter, Stuart expresses his concern and anxiety over the news that his "old lady" is not well, and hopes to receive another letter from home. He discusses a his business plans as well as news from a Presbyterian Theological Society camp meeting.
Date: November 4, 1832
Creator: Stuart, James
Item Type: Refine your search to only Letter
Partner: UNT Libraries Special Collections
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[Letter from Hamilton K. Redway to Loriette Redway, November 4, 1865]

Description: A letter from Hamilton K. Redway in Baltimore, Maryland to his wife, Loriette Redway, on November 4, 1865. In the letter, Hamilton Redway expresses his affection for his wife and family. He explains that though he would love to return home to his family, he would rather go into the army again in order to monetarily support his family. Redway asks about his father, Chauncey Redway, about Charles, and about Ellen. This could be in reference to his niece, Ellen Loretta. Also included with this i… more
Date: November 4, 1865
Creator: Redway, Hamilton K.
Item Type: Refine your search to only Letter
Partner: UNT Libraries Special Collections
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[Letter from Lula Dalton to Linnet Moore, November 4, 1899]

Description: Letter from Lula Dalton to Linnet Moore in which she expresses how much she misses Linnet. She says that Leta Fowler is to be married. She also writes about the new clothes she has had made or altered for he winter wardrobe. She also writes about Jim Cooke. The Floral Society has plans to put up an exhibit.
Date: November 4, 1899
Creator: Dalton, Lula
Item Type: Refine your search to only Letter
Partner: UNT Libraries Special Collections
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[Pension notification, November 4, 1916]

Description: A formal notification of pension increase to be attached to pension certificate. This notification details that Mrs. L. C. Redway's pension was increased to $20.00 per month under the Act of September 8, 1916.
Date: November 4, 1916
Creator: United States. Pension Bureau.
Item Type: Refine your search to only Text
Partner: UNT Libraries Special Collections
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General Potential Theory of Arbitrary Wing Sections

Description: The problem of determining the two dimensional potential flow around wing sections of any shape is examined. The problem is condensed into the compact form of an integral equation capable of yielding numerical solutions by a direct process. An attempt is made to analyze and coordinate the results of earlier studies relating to properties of wing sections. The existing approximate theory of thin wing sections and the Joukowski theory with its numerous generalizations are reduced to special cases… more
Date: November 4, 1932
Creator: Theodorsen, T. & Garrick, I. E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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Flying Qualities of a High-Speed Bomber With a Dual Pusher Propeller Aft of the Empennage as Estimated From Wind-Tunnel Tests of a 1/8-Scale Powered Model

Description: Report discussing the flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage. The airplane was found to have satisfactory flying qualities except for stability issues with aft center of gravity, high elevator control forces in landing, insufficient elevator control in take-off, and low rudder-free directional stability.
Date: November 4, 1944
Creator: Weiberg, James A. & Schnurbusch, Alfred W.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
transcript

Franklin Delano Roosevelt; Thomas E. Dewey

Description: Side 1 contains a presidential campaign speech by President Franklin Delano Roosevelt at Fenway Park in Boston. Side 2 contains a presidential campaign speech by Republican nominee Thomas E. Dewey at Madison Square Gardens in New York City. Dewey is introduced by announcer Ford Bond, and his speech was carried on the Mutual network.
Date: November 4, 1944
Duration: 31 minutes 06 seconds
Creator: Roosevelt, Franklin D. (Franklin Delano), 1882-1945 & Dewey, Thomas E. (Thomas Edmund), 1902-1971
Item Type: Refine your search to only Sound
Partner: UNT Music Library
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The Effect of Boundary-Layer Control by Suction and Several High-Lift Devices on the Longitudinal Aerodynamic Characteristics of a 47.5 Degree Sweptback Wing-Fuselage Combination

Description: "An investigation has been made in the Langley full-scale tunnel of a 47.5 degree sweptback wing-fuselage combination equipped for boundary-layer control by suction. The wing aspect ratio was 3.5, the taper ratio was 0.5, and the airfoil sections normal to the quarter-chord line were NACA 64(sub 1)-A112. The wing configurations tested included the wing with various combinations of extensible leading-edge and split flaps" (p. 1).
Date: November 4, 1948
Creator: Pasamanick, Jerome & Proterra, Anthony J.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

High-speed wind-tunnel tests of a 1/16-scale model of the D-558 research airplane-dynamic pressure and comparison of point and effective downwash at the tail of the D-558-1

Description: Report discussing the point downwash angles and dynamic pressure at the horizontal-tail location of the D-558-1 airplane at a range of Mach numbers and lift coefficients. Results regarding the effective downwash with the tail-on and tail-off configuration, flow direction at the tail, rate of change, and dynamic pressure changes are provided.
Date: November 4, 1948
Creator: Robinson, Harold L.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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Measurements in Flight of the Longitudinal-Stability Characteristics of a Republic YF-84A Airplane (Army Serial No. 45-59488) at High Subsonic Mach Numbers

Description: A brief investigation was made of the longitudinal-stability characteristics of a YF-84A airplane (Army Serial No. 45-79488). The airplane developed a pitching-up tendency at approximately 0.80 Mach number which necessitated large push forces and down-elevator deflections for further increases in speed. In steady turns at 35,000 feet with the center of gravity at 28.3 percent mean aerodynamic chord for normal accelerations up to the maximum test value, the control-force gradients were excessive… more
Date: November 4, 1948
Creator: Turner, Howard L. & Cooper, George E.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
open access

Analysis and Experimental Observation of Pressure Losses in Ram-Jet Combustion Chambers

Description: From Introduction: "Some experimental data on flame-holder pressure losses have been presented (reference 1 to 4). A theoretical analysis that assume a sudden enlargement of flow area was made at the NACA Lewis laboratory to determine the effect of flame-holder open area and combustion-chamber-inlet Mach number on the pressure losses across flame holders. The results of this analysis were then compared with experimental data obtained with several different flame-holder designs."
Date: November 4, 1949
Creator: Sterbentz, William H.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department
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