Detonation in the internal-combustion engine is studied as a physical process. It is shown that detonation is accompanied by pressure waves within the cylinder charge. Sound theory is applied to the calculation of resonant pressure-wave frequencies. Apparatus is described for direct measurement of pressure-wave frequencies. Frequencies determined from two engines of different cylinder sizes are shown to agree with the values calculated from sound theory. An outline of the theoretically possible modes of vibration in a right circular cylinder with flat ends is included. An appendix by John P. Elting gives a method of calculating pressure in the sound wave following detonation
Tangential mode, non-linear wave motion in a liquid propellant rocket engine is studied, using a two...
The theory of imploding detonations predicts a focusing effect by which the temperature, the pressur...
The object of the investigation presented in this report was to determine the effects of increasing ...
Detonation in the internal-combustion engine is studied as a physical process. It is shown that deto...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Physics, 1938.Includes bibliographi...
Axial and hoop stress calculation in blast loaded thin walled cylindrical pressure vessel
Measurements of rotating pressure wave about combustion chamber axis during resonant combustion of l...
Simultaneous direct and Schlieren photographs at 40,000 frames per second and correlated pressure re...
The expansion of air tra±c operations is nowadays limited by environmental constraints on noise. Adv...
This report presents the results of an investigation to determine experimentally the instantaneous p...
Reaction engine operates on the principles of a controlled condensed detonation rather than on the p...
An investigation conducted to determine the factors which control the combustion in a high-speed com...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
This report derives equations containing only directly measurable constants for the quantities invol...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Tangential mode, non-linear wave motion in a liquid propellant rocket engine is studied, using a two...
The theory of imploding detonations predicts a focusing effect by which the temperature, the pressur...
The object of the investigation presented in this report was to determine the effects of increasing ...
Detonation in the internal-combustion engine is studied as a physical process. It is shown that deto...
Thesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Physics, 1938.Includes bibliographi...
Axial and hoop stress calculation in blast loaded thin walled cylindrical pressure vessel
Measurements of rotating pressure wave about combustion chamber axis during resonant combustion of l...
Simultaneous direct and Schlieren photographs at 40,000 frames per second and correlated pressure re...
The expansion of air tra±c operations is nowadays limited by environmental constraints on noise. Adv...
This report presents the results of an investigation to determine experimentally the instantaneous p...
Reaction engine operates on the principles of a controlled condensed detonation rather than on the p...
An investigation conducted to determine the factors which control the combustion in a high-speed com...
The problem of determining the stability of high-frequency pressure oscillations in rocket combustio...
This report derives equations containing only directly measurable constants for the quantities invol...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Tangential mode, non-linear wave motion in a liquid propellant rocket engine is studied, using a two...
The theory of imploding detonations predicts a focusing effect by which the temperature, the pressur...
The object of the investigation presented in this report was to determine the effects of increasing ...