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  Partner: UNT Libraries Government Documents Department
 Year: 1945
 Month: July
Airspeed fluctuations as a measure of atmospheric turbulence

Airspeed fluctuations as a measure of atmospheric turbulence

Date: July 1, 1945
Creator: Tolefson, H B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of life expectancy of airplane wings in normal cruising flight

An analysis of life expectancy of airplane wings in normal cruising flight

Date: July 1, 1945
Creator: Putnam, Abbott A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Axial fatigue test at two stress amplitudes of 0.032-inch 24S-T sheet specimens with a circular hole

Axial fatigue test at two stress amplitudes of 0.032-inch 24S-T sheet specimens with a circular hole

Date: July 1, 1945
Creator: Brueggeman, W C; Mayer, M , Jr & Smith, W H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Blade design data for axial-flow fans and compressors

Blade design data for axial-flow fans and compressors

Date: July 1, 1945
Creator: Bogdonoff, Harriet E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : extruded 24S-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded 24S-T aluminum alloy

Date: July 1, 1945
Creator: Roy, J Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Column and Plate Compressive Strengths of Aircraft Structural Materials: Extruded 24S-T Aluminum Alloy

Date: July 1, 1945
Creator: Heimerl, George J. & Roy, J Albert
Description: Column and plate compressive strengths of extruded 24S-T aluminum alloy were determined both within and beyond the elastic range from tests of thin-strip columns and local-instability tests of H-, Z-,and channel-section columns. These tests are part of an extensive research investigation to provide data on the' structural strength of various aircraft materials. The results are presented in the form of curves and charts that are suitable for use in the design and analysis of aircraft structures.
Contributing Partner: UNT Libraries Government Documents Department
Column and plate compressive strengths of aircraft structural materials : extruded 75S-T aluminum alloy

Column and plate compressive strengths of aircraft structural materials : extruded 75S-T aluminum alloy

Date: July 1, 1945
Creator: Roy, J Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Comparison of structural efficiencies of diagonal-tension webs and truss webs of 24S-T aluminum alloy

Date: July 1, 1945
Creator: Ochiltree, David W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane

Date: July 1, 1945
Creator: Skoog, Richard B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Control of cylinder temperatures by thermostatically operated internal-coolant valves

Control of cylinder temperatures by thermostatically operated internal-coolant valves

Date: July 1, 1945
Creator: Miller, George R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The development and application of high-critical-speed nose inlets

The development and application of high-critical-speed nose inlets

Date: July 1, 1945
Creator: Wright, John B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Domestic disturbances

Domestic disturbances

Date: July 30, 1945
Creator: United States. War Department.
Description: "This manual presents the principles for the employment of troops during domestic disturbances and the essential substances of the more important laws relating to the employment of military forces in the aid of civil authorities with the applicable War Department policies"
Contributing Partner: UNT Libraries Government Documents Department
Economy of internally cooling only the overheated cylinders of aircraft engines

Economy of internally cooling only the overheated cylinders of aircraft engines

Date: July 1, 1945
Creator: Henneberry, Hugh M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of blade loading of the climb and high-speed performance of a three-blade Hamilton standard no. 6507A-2 propeller on a Republic P-47D airplane

Effect of blade loading of the climb and high-speed performance of a three-blade Hamilton standard no. 6507A-2 propeller on a Republic P-47D airplane

Date: July 1, 1945
Creator: Gardner, John J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil

Date: July 1, 1945
Creator: Bird, J D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing

Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing

Date: July 6, 1945
Creator: Blair, William K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of some design parameters on ditching characteristics

The effect of some design parameters on ditching characteristics

Date: July 1, 1945
Creator: Dawson, John R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of the lift coefficient on propeller flutter

Effect of the lift coefficient on propeller flutter

Date: July 1, 1945
Creator: Regier, Arthur A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An Experimental Investigation of the Effect of Propellers Used as Aerodynamic Brakes on Stability and Control

An Experimental Investigation of the Effect of Propellers Used as Aerodynamic Brakes on Stability and Control

Date: July 1, 1945
Creator: Hanson, Frederick H
Description: Tests were made of a model representative of a single-engine tractor-type airplane for the purpose of determining the stability and control effects of a propeller used as an aerodynamic brake. The tests were made with single-and dual-rotation propellers to show the effect of type of propeller rotation, and with positive thrust to provide basic data with which to compare the effects of negative thrust. Four configurations of the model were used to give the effects of tilting the propeller thrust axis down 5 deg., raising the horizontal tail, and combining both tilt and raised tail. Results of the tests are reported herein. The effects of negative thrust were found to be significant. The longitudinal stability was increased because of the loss of wing lift and increase of the angle of attack of the tail. Directional stability and both longitudinal and directional control were decreased because of the reduced velocity at the tail. These effects are moderate for moderate braking but become pronounced with full-power braking, particularly at high values of lift coefficient. The effects of model configuration changes were small when compared with the over-all effects of negative-thrust operation; however, improved stability and control characteristics were exhibited by the model ...
Contributing Partner: UNT Libraries Government Documents Department
Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines I : determination of the cooling characteristics of the flight engine

Flight and test-stand investigation of high-performance fuels in modified double-row radial air-cooled engines I : determination of the cooling characteristics of the flight engine

Date: July 1, 1945
Creator: White, H Jack
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Gas Injection into the McClosky Limestone in the Griffin and New Harmony Oil Fields, Indiana and Illinois

Gas Injection into the McClosky Limestone in the Griffin and New Harmony Oil Fields, Indiana and Illinois

Date: July 1945
Creator: Riggs, C. H.
Description: Report issued by the U.S. Bureau of Mines conducted a study on the injection of gas into the McClosky limestone in northern Illinois and Indiana. The resulting increases in oil and gas production from this area are presented. The report includes maps, graphs, tables, and illustrations.
Contributing Partner: UNT Libraries Government Documents Department
Inspection and preventive maintenance services for kitchen equipment.

Inspection and preventive maintenance services for kitchen equipment.

Date: July 1945
Creator: United States. War Department.
Description: "This Technical Manual describes the inspections and services necessary to maintain the efficiency and prolong the life of kitchen equipment."
Contributing Partner: UNT Libraries Government Documents Department
Investigation of a method of comparison of metallic surface contours by means of stereoscopic electron micrographs

Investigation of a method of comparison of metallic surface contours by means of stereoscopic electron micrographs

Date: July 1, 1945
Creator: Shaw, Milton C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurement of flying qualities of a DeHavilland Mosquito F-8 airplane (AAF No. 43-334960) II : longitudinal stability and control characteristics

Measurement of flying qualities of a DeHavilland Mosquito F-8 airplane (AAF No. 43-334960) II : longitudinal stability and control characteristics

Date: July 1, 1945
Creator: Gray, W E , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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