Serial/Series Title

Corrugated Metal Diaphragms for Aircraft Pressure-Measuring Instruments (open access)

Corrugated Metal Diaphragms for Aircraft Pressure-Measuring Instruments

Note presenting a description of a large number of corrugated diaphragms of beryllium copper, phosphor bronze, and Z-nickel with geometrically similar outlines but various diameters and thicknesses were formed by hydraulic pressing. The apparatus and technique used in the manufacture, testing, and heat treatment are described. Results regarding pressure-deflection curves, load limit, effect of center reinforcing, snap-action diaphragms, deflection traverse, thickness variations, and concentrated central loads are provided.
Date: November 1939
Creator: Wildhack, W. A. & Goerke, V. H.
System: The UNT Digital Library
Photoelastic Analysis of Three-Dimensional Stress Systems Using Scattered Light (open access)

Photoelastic Analysis of Three-Dimensional Stress Systems Using Scattered Light

"A method has been developed for making photoelastic analyses of three-dimensional stress systems by utilizing the polarization phenomena associated with the scattering of light. By this method, the maximum shear and the directions of the three principal stresses at any point within a model can be determined, and the two principal stresses at a free-bounding surface can be separately evaluated. Polarized light is projected into the model through a slit so that it illuminates a plane section" (p. 1).
Date: November 1939
Creator: Weller, R. & Bussey, J. K.
System: The UNT Digital Library
Pressure-Distribution Investigation of an N.A.C.A. 0009 Airfoil With a 50-Percent-Chord Plain Flap and Three Tabs (open access)

Pressure-Distribution Investigation of an N.A.C.A. 0009 Airfoil With a 50-Percent-Chord Plain Flap and Three Tabs

"Pressure-distribution tests of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three plain tabs, having chords 10, 20, and 30 percent of the flap chord, were made in the N.A.C.A. 4- by 6- foot vertical tunnel. The tests supplied aerodynamic section data that may be applied to the design of horizontal and vertical tail surfaces. The results are presented as resultant-pressure diagrams for the airfoil with the flap and the 20-percent-chord tab" (p. 1).
Date: November 1939
Creator: Street, William G. & Ames, Milton B., Jr.
System: The UNT Digital Library
Pressure-Distribution Measurements on a Tapered Wing With a Partial-Span Split Flap in Curved Flight (open access)

Pressure-Distribution Measurements on a Tapered Wing With a Partial-Span Split Flap in Curved Flight

"Pressure-distribution tests were made on the 32-foot whirling arm of the Daniel Guggenheim Airship Institute of a tapered wing to determine the rolling and the yawing moments due to an angular velocity in yaw. The model was tested at 0 degree and 5 degree pitch; 0 degree, 5 degree, and 10 degree yaw; and with split flaps covering 25, 50, 75, and 100 percent of the wing span and deflected 60 degrees. The results are given in the form of load distributions and as calculated moment coefficients" (p. 1).
Date: November 1939
Creator: Troller, T. & Rokus, F.
System: The UNT Digital Library
Tidewater and Weather-Exposure Tests on Metals Used in Aircraft (open access)

Tidewater and Weather-Exposure Tests on Metals Used in Aircraft

"Tidewater and weather-exposure tests on various aluminum alloys, magnesium alloys, and stainless steels are now being conducted by the National Bureau of Standards. Exposures were begun in June 1938 and, according to present plans, are to continue over a 3-year period. The methods of exposure and the materials being investigated are described and the more important results obtained up to the conclusion of the first year's exposure are reported" (p. 1).
Date: November 1939
Creator: Mutchler, Willard & Galvin, W. G.
System: The UNT Digital Library