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  Partner: UNT Libraries Government Documents Department
 Decade: 1940-1949
 Year: 1942
 Month: July
 Collection: Technical Report Archive and Image Library
Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

Date: July 1, 1942
Creator: Goranson, R Fabian
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calibrations of pitot-static tubes at high speeds

Calibrations of pitot-static tubes at high speeds

Date: July 1, 1942
Creator: Hensley, Reece V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Column strength of magnesium alloy AM-57S

Column strength of magnesium alloy AM-57S

Date: July 1, 1942
Creator: Holt, M
Description: Tests were made to determine the column strength of extruded magnesium alloy AM-57S. Column specimens were tested with round ends and with flat ends. It was found that the compressive properties should be used in computations for column strengths rather than the tensile properties because the compressive yield strength was approximately one-half the tensile yield strength. A formula for the column strength of magnesium alloy AM-57S is given.
Contributing Partner: UNT Libraries Government Documents Department
Determination of the stability and control characteristics of airplanes from tests of powered models

Determination of the stability and control characteristics of airplanes from tests of powered models

Date: July 1, 1942
Creator: Swanson, Robert S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Diagrams for calculation of airfoil lattices

Diagrams for calculation of airfoil lattices

Date: July 1, 1942
Creator: Betz, Albert
Description: The field for curved blades is represented by a vortex series with a vortex removed at the blade point. Further, an example of calculation of a curved blade from this series is given, whereby the necessary accuracy required of the different methods in practice is shown according to the case considered.
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of a new type of low-drag wing-nacelle combination

Experimental investigation of a new type of low-drag wing-nacelle combination

Date: July 1, 1942
Creator: Allen, H. J. & Frick, C. W., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight investigation of a stall-warning indicator for operation under icing conditions

Flight investigation of a stall-warning indicator for operation under icing conditions

Date: July 1, 1942
Creator: Zalovcik, John A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Generalized selection charts for bombers powered by one, two, four, and six 2000-horsepower engines

Generalized selection charts for bombers powered by one, two, four, and six 2000-horsepower engines

Date: July 1, 1942
Creator: Hill, Paul R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed wind-tunnel tests of gun openings in the nose of the fuselage of a 1/4-scale model

High-speed wind-tunnel tests of gun openings in the nose of the fuselage of a 1/4-scale model

Date: July 1, 1942
Creator: Fedziuk, Henry A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of means for extending the range of several bombers to 6000 miles

Investigation of means for extending the range of several bombers to 6000 miles

Date: July 1, 1942
Creator: Harmon, S M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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