This report presents the results of an analytical investigation on the practicability of using mechanically operated discharge valves in conjunction with a manually operated intake control for improving the performance of N. A. C. A. Roots type superchargers. These valves, which may be either of the oscillating or rotating type, are placed in the discharge opening of the supercharger and are so shaped and synchronized with the supercharger impellers that they do not open until the air has been compressed to the delivery pressure. The intake control limits the quantity of air compressed to engine requirements by permitting the excess air to escape from the compression chamber before compression begins. The percentage power saving and the act...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
This report presents the comparative flight results of a roots supercharger and a turbocentrifugal s...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
This report presents the results of an analytical investigation on the practicability of using mecha...
This report presents a comparison of superchargers on the basis of the power required to compress th...
This report presents the results of tests of a Power plus supercharger and a comparison of its perfo...
This report describes a roots type aircraft engine supercharger and presents the results of some tes...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
With the aid of simple considerations and test results, an attempt is made to clear up some obscure ...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
Various methods of providing compressor-capacity and pressure-ratio control in the gas-generator typ...
As part of an investigation to increase the power output of the V-1710-93 engine at altitude, the en...
This report presents the results of an investigation to determine the effect of different supercharg...
.kn investigation of hhe suitability of the X. A. C..4. Roots type aircraft erigitte super-charger t...
The object of the investigation presented in this report was to determine the effects of increasing ...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
This report presents the comparative flight results of a roots supercharger and a turbocentrifugal s...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...
This report presents the results of an analytical investigation on the practicability of using mecha...
This report presents a comparison of superchargers on the basis of the power required to compress th...
This report presents the results of tests of a Power plus supercharger and a comparison of its perfo...
This report describes a roots type aircraft engine supercharger and presents the results of some tes...
In part one of this report are presented the theoretical performance curves of an airplane engine eq...
With the aid of simple considerations and test results, an attempt is made to clear up some obscure ...
Discussed here are the principles and operation of aircraft engine superchargers used to maintain an...
Various methods of providing compressor-capacity and pressure-ratio control in the gas-generator typ...
As part of an investigation to increase the power output of the V-1710-93 engine at altitude, the en...
This report presents the results of an investigation to determine the effect of different supercharg...
.kn investigation of hhe suitability of the X. A. C..4. Roots type aircraft erigitte super-charger t...
The object of the investigation presented in this report was to determine the effects of increasing ...
The Rateau supercharger investigated had, under normal operating conditions, an adiabatic efficiency...
This report presents the comparative flight results of a roots supercharger and a turbocentrifugal s...
In terminating the study of the adaptation of the engine to the airplane, we will examine the proble...