Serial/Series Title

Month

Analysis of Circular Shell-Supported Frames (open access)

Analysis of Circular Shell-Supported Frames

From Summary: "This paper deals with the single problem if circular shell-supported frames subjected to concentrated loadings. A mathematical attack is developed and presented in the form of nondimensional-coefficient curves."
Date: May 1944
Creator: Wignot, J. E.; Combs, Henry & Ensrud, A. F.
System: The UNT Digital Library
Plastic Mountings for Aircraft Windshields (open access)

Plastic Mountings for Aircraft Windshields

Note presenting an investigation of several laminated glass windshields to determine their suitability for use in airplanes with pressurized cabins. The various constructions of the extended portions of the windshields which serve for mounting purposes included plastic alone, plastic and one sheet of glass extended, plastic extension reinforced with an aluminum strip, and plastic extension reinforced with a steel strip. The results indicated that the laminated windshields with plastic-mounting extensions reinforced by aluminum or steel were resistant to creep and bursting at pressures of the order that will be encountered in service.
Date: May 1944
Creator: Bradley, Kathryn H. & Axilrod, B. M.
System: The UNT Digital Library
The numerical solution of compressible fluid flow problems (open access)

The numerical solution of compressible fluid flow problems

Numerical methods have been developed for obtaining the steady, adiabatic flow field of a frictionless, perfect gas about arbitrary two-dimensional bodies. The solutions include the subsonic velocity regions, the supersonic velocity regions, and the transition compression shocks, if required. Furthermore, the rotational motion and entropy changes following shocks are taken into account. Extensive use is made of the relaxation method. In this report the details of the methods of solution are emphasized so as to permit others to solve similar problems. Solutions already obtained are mentioned only by way of illustrating the possibilities of the methods described. The methods can be applied directly to wind tunnel and free air tests of arbitrary airfoil shapes at subsonic, sonic, and supersonic speeds.
Date: May 1944
Creator: Emmons, Howard W.
System: The UNT Digital Library
Charts for rapid analysis of 45 degree strain-rosette data (open access)

Charts for rapid analysis of 45 degree strain-rosette data

From Summary: "Charts are presented for rapidly determining the principal strains and stresses, the maximum shear strain and stress, and the orientation of principal axes from data on 45 degree strain rosettes. The charts may be used for analyzing the conventional data consisting of strains measured along three gage lines 45 degrees apart, but their application is more direct if the rosette data are obtained by means of special circuits that require the use of four gages 45 degrees apart."
Date: May 1944
Creator: Manson, S. S.
System: The UNT Digital Library
An automatic electrical analyzer for 45 degree strain-rosette data (open access)

An automatic electrical analyzer for 45 degree strain-rosette data

Report presenting a device that automatically analyses the data from a 45 degree strain rosette. The rosette strains are properly combined by means of an electric circuit to yield a direct meter reading of maximum shear strain and major and minor principal strains.
Date: May 1944
Creator: Manson, S. S.
System: The UNT Digital Library