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Disturbing Effect of Free Hydrogen on Fuel Combustion in Internal Combustion Engines

Description: "Experiments with fuel mixtures of varying composition, have recently been conducted by the Motor Vehicle and Airplane Engine Testing Laboratories of the Royal Technical High School in Berlin and at Fort Hahneberg, as well as at numerous private engine works. The behavior of hydrogen during combustion in engines and its harmful effect under certain conditions, on the combustion in the engine cylinder are of general interest. Some of the results of these experiments are given here, in order to e… more
Date: March 1923
Creator: Riedler, A.
Partner: UNT Libraries Government Documents Department
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Notes on Aerodynamic Forces on Airship Hulls

Description: "For a first approximation the air flow around the airship hull is assumed to obey the laws of perfect (i.e. free from viscosity) incompressible fluid. The flow is further assumed to be free from vortices (or rotational motion of the fluid). These assumptions lead to very great simplifications of the formulae used but necessarily imply an imperfect picture of the actual conditions. The value of the results depends therefore upon the magnitude of the forces produced by the disturbances in the fl… more
Date: March 1923
Creator: Tuckerman, L. B.
Partner: UNT Libraries Government Documents Department
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Standardization and Aerodynamics

Description: Report presenting suggestions for the standardization of the study of aerodynamics in laboratories in the United States and Europe. A report by each of the different scientists, all of whom are working in a variety of different labs and countries, is provided, and each discusses the progress made in their respective labs and their suggestions for standardization and progress in the field.
Date: March 1923
Creator: Knight, William; Prandtl, L.; von Karman; Costanzi, G.; Margoulis, W.; Verduzio, R. et al.
Partner: UNT Libraries Government Documents Department
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Variation in the Number of Revolutions of Air Propellers

Description: Note describing the variation in the number of revolutions per minute and provides simple formulas that allow for advanced calculation to be made of the variation of propeller speed with variation of one or more dimensions of the propeller and allow the necessary corrections to be applied.
Date: March 1923
Creator: Achenbach, W.
Partner: UNT Libraries Government Documents Department
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