Methods for the Identification of Aircraft Tubing of Plain Carbon Steel and Chromium-Molybdenum Steel (open access)

Methods for the Identification of Aircraft Tubing of Plain Carbon Steel and Chromium-Molybdenum Steel

The survey of the possibilities for distinguishing between plain carbon and chromium-molybdenum steel tubing included the Herbert pendulum hardness, magnetic, sparks, and chemical tests. The Herbert pendulum test has the disadvantages of all hardness tests in being limited to factory use and being applicable only to scale-free, normalized material. The small difference in the range of hardness values between plain carbon and chromium-molybdenum steels is likewise a disadvantage.
Date: October 1930
Creator: Mutchler, W. H. & Buzzard, R. W.
System: The UNT Digital Library
An Accurate Method of Measuring the Moments of Inertia of Airplanes (open access)

An Accurate Method of Measuring the Moments of Inertia of Airplanes

From Summary: "This note contains a description of an improved apparatus and procedure used by the NACA for determining the moments of inertia of airplanes. The method used, based on the pendulum theory, is similar to that previously used, but a recent investigation of its accuracy has resulted in the improvements described herein. The error, when using the new apparatus and procedure, has been found to be of the order of 1 per cent."
Date: October 1930
Creator: Miller, M. P.
System: The UNT Digital Library
Effect of Orifice Length-Diameter Ratio on Spray Characteristics (open access)

Effect of Orifice Length-Diameter Ratio on Spray Characteristics

"The effect of variations of orifice length to diameter ratio on spray characteristics was determined for a 0.014-inch and a 0.040-inch orifice for ratio of 0.5 to 4.0. The nozzles containing the orifices were mounted in an injection valve and tested with a plan stem and with a helically grooved stem. The injection pressure was varied from 4000 to 8000 pounds per square inch. The air density into which the fuel was sprayed was varied from the density obtained with a pressure of 60 pounds per square inch to the density obtained with a pressure of 250 pounds per square inch at room temperature" (p. 1).
Date: October 1930
Creator: Gelalles, A. G.
System: The UNT Digital Library
Analytical Determination of the Load on a Trailing Edge Flap (open access)

Analytical Determination of the Load on a Trailing Edge Flap

From Summary: "This report presents a theoretical analysis of the lift on a trailing edge flap. An analytical expression has been derived which enables the computation of the flap load coefficient. The theoretical results seem to show a fair agreement with the meager experimental results which are available."
Date: October 1930
Creator: Pinkerton, Robert M.
System: The UNT Digital Library