Formulas are derived for computing the instantaneous pressures delivered by a fuel pump. The first derivation considers the compressibility of the fuel and the second, the compressibility, elasticity, and inertia of the fuel. The second derivation follows that given by Sass; it is shown to be the more accurate of the two. Additional formulas are given for determining the resistance losses in the injection tube. Experimental data are presented in support of the analyses. The report is concluded with an application of the theory to the design of fuel pump injection systems for which sample calculations are included
In connection with the development of a method for analyzing indicator cards taken from high-speed c...
Using the method of weighing fuel collected in a receiver during a definite interval of the injectio...
Two methods were used to measure fuel distribution within sprays from several types of fuel-injectio...
The tests discussed in this report were conducted to determine whether or not there is appreciable v...
This report presents the results of an investigation to determine experimentally the instantaneous p...
This report summarizes some results obtained with a single cylinder test engine at the Langley Field...
An investigation conducted to determine the factors which control the combustion in a high-speed com...
The effects of air flow on fuel spray and flame formation in a high-speed compression-ignition engin...
Test data and analysis show that the rate of fuel leakage between a lapped plunger and sleeve varies...
The object of the investigation presented in this report was to determine the effects of increasing ...
This investigation was undertaken at the Langley Memorial Aeronautical Laboratory in connection with...
This research on the pressure variations in the injection system of the N.A.C.A. Spray Photography E...
This report presents the results of a study made of the influence of several variables on the pressu...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Formulas are derived for computing the instantaneous pressures delivered by a fuel pump. The first d...
In connection with the development of a method for analyzing indicator cards taken from high-speed c...
Using the method of weighing fuel collected in a receiver during a definite interval of the injectio...
Two methods were used to measure fuel distribution within sprays from several types of fuel-injectio...
The tests discussed in this report were conducted to determine whether or not there is appreciable v...
This report presents the results of an investigation to determine experimentally the instantaneous p...
This report summarizes some results obtained with a single cylinder test engine at the Langley Field...
An investigation conducted to determine the factors which control the combustion in a high-speed com...
The effects of air flow on fuel spray and flame formation in a high-speed compression-ignition engin...
Test data and analysis show that the rate of fuel leakage between a lapped plunger and sleeve varies...
The object of the investigation presented in this report was to determine the effects of increasing ...
This investigation was undertaken at the Langley Memorial Aeronautical Laboratory in connection with...
This research on the pressure variations in the injection system of the N.A.C.A. Spray Photography E...
This report presents the results of a study made of the influence of several variables on the pressu...
Report presents the results of performance tests of a single-cylinder 4-stroke-cycle compression-ign...
Formulas are derived for computing the instantaneous pressures delivered by a fuel pump. The first d...
In connection with the development of a method for analyzing indicator cards taken from high-speed c...
Using the method of weighing fuel collected in a receiver during a definite interval of the injectio...
Two methods were used to measure fuel distribution within sprays from several types of fuel-injectio...