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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results of a Biological Survey of the San Francisco Mountain Region and Desert of the Little Colorado, Arizona

Results of a Biological Survey of the San Francisco Mountain Region and Desert of the Little Colorado, Arizona

Date: September 11, 1890
Creator: Merriam, C. Hart & Stejneger, Leonhard
Description: Brief summary of a biological survey of the Painted Desert, specifically the San Francisco Mountain region, and the Grand Canyon (Cañon).
Contributing Partner: UNT Libraries Government Documents Department
Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6

Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6

Date: April 1, 1956
Creator: Welsh, Clement J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of a Force Test of Four Configurations of the Hi-Lo Instrumented and Chaff Rockets in the Sandia Corporation 12 x 12 inch Transonic Wind Tunnel (Program III-46)

Results of a Force Test of Four Configurations of the Hi-Lo Instrumented and Chaff Rockets in the Sandia Corporation 12 x 12 inch Transonic Wind Tunnel (Program III-46)

Date: September 24, 1959
Creator: Arnold, J. W.
Description: Abstract: Force, moment, and center of pressure information are presented for four models of the Hi-Lo configuration.
Contributing Partner: UNT Libraries Government Documents Department
Results of a power-on flight of a 1/10-scale rocket-propelled model of the convair xf2y-1 airplane at a mach number of 1.53

Results of a power-on flight of a 1/10-scale rocket-propelled model of the convair xf2y-1 airplane at a mach number of 1.53

Date: January 1, 1953
Creator: Bland, W. M., Jr. & Nelson, R. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of a rocket-model investigation of control-surface buzz and flutter on a 4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings at transonic speeds

Results of a rocket-model investigation of control-surface buzz and flutter on a 4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings at transonic speeds

Date: November 20, 1953
Creator: Henning, Allen B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S.T. Ae.) of Rhode St. Genese, Brussels

Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S.T. Ae.) of Rhode St. Genese, Brussels

Date: February 1, 1928
Creator: Puvrez, Paul
Description: We have investigated the maximum lift obtainable with slotted airfoils derived from a symmetrical airfoil. These should have a smaller profile drag than other slotted airfoils.
Contributing Partner: UNT Libraries Government Documents Department
Results of Air-Water and Steam-Water Tests on Radial Vane Steam Separator Models

Results of Air-Water and Steam-Water Tests on Radial Vane Steam Separator Models

Date: February 1962
Creator: Riesland, J. I.
Description: From introduction: "Describes progress in the development of radial vane primary separators following initial work reported in GEAP 3564."
Contributing Partner: UNT Libraries Government Documents Department
Results of an Airborne Radiometric Survey in the Canon City Embayment Area, Colorado

Results of an Airborne Radiometric Survey in the Canon City Embayment Area, Colorado

Date: June 16, 1954
Creator: Nash, A. L. & Brown, L. J.
Description: Abstract: An airborne radiometric survey of the Dakota sandstone and Morrison formation in the Canon City embayment was conducted by the Atomic Energy Commission from November 1, 1953 to December 5, 1953.
Contributing Partner: UNT Libraries Government Documents Department
Results of an experimental investigation of small viscous dampers

Results of an experimental investigation of small viscous dampers

Date: June 1, 1958
Creator: Silveira, Milton A; Maglieri, Domenic J & Brooks, George W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of an investigation at high subsonic speeds to determine lateral-control and hinge-moment characteristics of a spoiler-slot-deflector configuration on a 35 degree sweptback wing

Results of an investigation at high subsonic speeds to determine lateral-control and hinge-moment characteristics of a spoiler-slot-deflector configuration on a 35 degree sweptback wing

Date: June 5, 1957
Creator: Hammond, Alexander D & Brown, Albert E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of Assays of the New Albany Oil-Shale

Results of Assays of the New Albany Oil-Shale

Date: June 1923
Creator: Reeves, John R.
Description: Report issued by the U.S. Bureau of Mines on a survey of the New Albany oil-shale deposits in Indiana. The experimental procedures for surveying and sampling these shale deposits are presented in detail. This report includes tables, and graphs.
Contributing Partner: UNT Libraries Government Documents Department
Results of ATR Sample Fuel Plate Irradiation Experiment

Results of ATR Sample Fuel Plate Irradiation Experiment

Date: March 23, 1964
Creator: Phillips Petroleum Company
Description: From abstract: "Fuel materials proposed for use in the Advanced Test Reactor were evaluated."
Contributing Partner: UNT Libraries Government Documents Department
Results of axial-load fatigue tests on electropolished 2024-T3 and 7075-T6 aluminum-alloy-sheet specimens with central holes

Results of axial-load fatigue tests on electropolished 2024-T3 and 7075-T6 aluminum-alloy-sheet specimens with central holes

Date: March 1, 1956
Creator: Landers, Charles B & Hardrath, Herbert F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of edge-compression on stiffened flat-sheet panels of alclad and nonclad 14S-T6, 24S-T3, and 75S-T6 aluminum alloys

Results of edge-compression on stiffened flat-sheet panels of alclad and nonclad 14S-T6, 24S-T3, and 75S-T6 aluminum alloys

Date: April 1, 1954
Creator: Holt, Marshall
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of Electrical Resistivity and Electrical Induction Measurements at Abana Mine, Quebec, Canada: Explanation of Some Factors Associated with Induction Method

Results of Electrical Resistivity and Electrical Induction Measurements at Abana Mine, Quebec, Canada: Explanation of Some Factors Associated with Induction Method

Date: 1931
Creator: Potter, E. Vernon & Lee, F. W.
Description: Technical paper issued by the Bureau of Mines over studies conducted on electrical resistivity at the Abana Mine in Quebec. The methods used, and results of the studies are discussed. This paper includes tables, maps, and illustrations.
Contributing Partner: UNT Libraries Government Documents Department
Results of experimental flights at high altitudes with Daimler, Benz and Maybach engines to determine mixture formation and heat utilization of fuel

Results of experimental flights at high altitudes with Daimler, Benz and Maybach engines to determine mixture formation and heat utilization of fuel

Date: January 1, 1923
Creator: Kutzbach, K
Description: The experimental flights described herein were made with the object of obtaining information regarding the following two questions, which as yet have not been sufficiently elucidated. These are: 1. What effect has altitude upon the formation of the mixture? 2. What alteration takes place, with increasing altitude, in the utilization of the heat contained in the fuel?.
Contributing Partner: UNT Libraries Government Documents Department
Results of experiments with slotted wings

Results of experiments with slotted wings

Date: October 1, 1924
Creator: Lachmann, G
Description: This report recounts some of the successful experiments conducted in England and Germany on slotted wings and ailerons. Wind tunnel test results are given and examples of aircraft constructed with these new wing components are described.
Contributing Partner: UNT Libraries Government Documents Department
Results of extended tests of the Focke-Wulf F 19a "ente," a tail-first airplane

Results of extended tests of the Focke-Wulf F 19a "ente," a tail-first airplane

Date: September 1, 1933
Creator: Hubner, Walter
Description: These investigations consisted chiefly of measurements of the take-off distance under various starting conditions and with the c.g. in different positions; of the climbing speed as a function of the impact pressure and location of the c.g.; of the longitudinal stability and fore-and-aft controllability and of the determination of the elevator forces and characteristics of the elevator control.
Contributing Partner: UNT Libraries Government Documents Department
Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat

Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat

Date: June 11, 1947
Creator: Seacord, Charles L., Jr. & Teitelbaum, J. M.
Description: The results of the first flight test of a swept-back four-wing version of Tiamat (MX-570 model C) which was launched at the NACA Pilotless Aircraft Research Station at W4110PB Island, Va. are presented. In general, the flight behavior was close to that predicted by calculations based an stability theory and oscillating table tests of the autopilot. The flight test thus indicates that the techniques employed to predict automatic stability are valid and practical from an operational viewpoint. The limitations of the method used to predict flight behavior arise from the fact that the calculations assume no coupling among roll, pitch, and yaw, while in actual flight some such coupling does exist.
Contributing Partner: UNT Libraries Government Documents Department
Results of flight tests at supersonic speeds to determine the effect of body nose fineness ratio on body and wing drag

Results of flight tests at supersonic speeds to determine the effect of body nose fineness ratio on body and wing drag

Date: June 26, 1947
Creator: Katz, Ellis R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of flight tests to determine drag of parabolic and cone-cylinder bodies of very large fineness ratios at supersonic speeds

Results of flight tests to determine drag of parabolic and cone-cylinder bodies of very large fineness ratios at supersonic speeds

Date: August 30, 1951
Creator: Welsh, Clement J & Demoraes, Carlos A
Description: Results of a free-flight investigation at supersonic speeds to determine zero-lift drag of a series of bodies of revolution are presented. Configurations tested included two parabolic bodies with fineness ratios of 17.78 and 24.5 and two 8 degree cone-cylinder bodies with fineness ratios of 17.2 and 21.2. Results of previous tests of similar parabolic bodies but with lower fineness ratios are included in this paper for comparison. All bodies for which data are presented in this paper had a base-to-maximum-diameter ratio of 0.437. Calculated drag coefficients are shown for all bodies for which data are presented. (author).
Contributing Partner: UNT Libraries Government Documents Department
Results of flight tests to determine the drag of finite-length cylinders at high Reynolds numbers for a Mach number range of 0.5 to 1.3

Results of flight tests to determine the drag of finite-length cylinders at high Reynolds numbers for a Mach number range of 0.5 to 1.3

Date: June 16, 1952
Creator: Welsh, Clement J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of free-flight test of 1/10-scale model of the Convair XF2Y-1 airplane between Mach numbers of 0.7 and 1.45, including power-on flight at Mach number 1.2 : TED No. NACA DE 365

Results of free-flight test of 1/10-scale model of the Convair XF2Y-1 airplane between Mach numbers of 0.7 and 1.45, including power-on flight at Mach number 1.2 : TED No. NACA DE 365

Date: February 4, 1954
Creator: Bland, William M , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of initial wind-tunnel flutter experiments at low speed with a towed airplane model having a 40 degree sweptback wing of aspect ratio 3.62 equipped with pylon-mounted stores

Results of initial wind-tunnel flutter experiments at low speed with a towed airplane model having a 40 degree sweptback wing of aspect ratio 3.62 equipped with pylon-mounted stores

Date: March 24, 1955
Creator: Martina, Albert P & Young, George E
Description: None
Contributing Partner: UNT Libraries Government Documents Department