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Udder Diseases of Dairy Cows

Description: "A cow that is healthy in every other respect, but has a diseased or nonproducing udder, is worthless in a dairy herd. The prevention and treatment of the diseases which bring about this condition are discussed in this bulletin. The limitations of a bulletin of this kind preclude anything more than a brief discussion of each disease and a suggested line of simple treatment adapted to the means and condition of the average dairyman." -- p. ii. Diseases discussed include inflammatory diseases, ab… more
Date: 1924
Creator: Bunyea, Hubert, 1885-1942
Item Type: Refine your search to only Pamphlet
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Ultra-Light Alloys and Their Utilization on Aircraft

Description: Memorandum presenting an overview of ultra-light alloys and their potential use on an aircraft. A definition of ultra-light alloys, some of the present possibilities of ultra-light alloys, and some of the principles governing the use of the alloys in aircraft are provided.
Date: May 1924
Creator: Portevin, A. M. & DeFleury, R.
Item Type: Refine your search to only Report
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The vector ruling protractor

Description: The theory, structure and working of a vector slide rule is presented in this report. This instrument is used for determining a vector in magnitude and position when given its components and its moment about a point in their plane.
Date: March 1924
Creator: Zahm, A. F.
Item Type: Refine your search to only Report
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The vertical, longitudinal, and lateral accelerations experienced by an S. E. 5a airplane while maneuvering

Description: "This investigation was carried out by the Langley Field Laboratory of the National Advisory Committee for Aeronautics for the purpose of measuring the accelerations along the three principal axes of an airplane while it was maneuvering. The airplane selected for this purpose was the fairly maneuverable SE-5A and the instruments used were the NACA three component accelerometer and the NACA recording airspeed meter. The results showed that the normal accelerations did not exceed 4.000 G. While t… more
Date: 1924
Creator: Norton, F. H. & Carroll, T.
Item Type: Refine your search to only Report
open access

Wind Tunnel Tests of Correction Formula for Wings of Large Span

Description: The theory (wing experiments in an artificial air stream are subject to error, due to the fact that the wing is not situated in an unlimited body of air) by means of which the given drag correction was obtained, was based on various assumptions (e.g., elliptical distribution of lift) which do not always hold true. For this reason it was desirable to test the equation for the additional drag in regard to its reliability and range of application.
Date: May 1924
Creator: Wieselsberger, C.
Item Type: Refine your search to only Report
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